UK National Archives at Kew
Directorate of Scientific Research (DSIR) Engine Records, 1914 - 1939
Compiled by David Birch - 19 Oct 2011
Reference | Title or Scope | Covering Dates | Former Ref |
DSIR 23/341 | Gnome engine: fractured connecting rods | 1914 | T 341 |
DSIR 23/374 | Royal Aircraft Factory: testing plant for aeronautical engines | 1914 | T 374 |
DSIR 23/394 | Gnome engine inlet valves: examination of two broken balance weights | 1914 | T 394 |
DSIR 23/398 | Gnome engine No. 2981: results of examination | 1914 | T 398 |
DSIR 23/408 | Austrian Daimler 120 H.P. engine: report on fractured crank-shaft | 1914 | T 408 |
DSIR 23/444 | Gnome engine: fractured nose plate | 1914 | T 444, 444a-c |
DSIR 23/489 | Renault engine No. 42795: fractured cylinder head sent by Army Council described as new engine which broke in half in the air | 1915 | T 489 |
DSIR 23/561 | Multiple-engined aeroplanes | 1915 | T 561 |
DSIR 23/631 | Air compressor for R.A.F. 1 engine | 1916 | T 631 |
DSIR 23/652 | Propellers for twin-engine machines: requests for opinion on failure of propeller on a Curtiss aeroplane | 1916 | T 652, 652a-b |
DSIR 23/661 | Sunbeam aero-engine: investigation of fracture of exhaust springs | 1916 | T 661 |
DSIR 23/773 | Cooling of aeroplane engine cylinders | 1916 | T 759 |
DSIR 23/808 | Cooling of aeroplane engine cylinders | 1916 | T 794, 794a-b |
DSIR 23/873 | Radiators for water-cooled engines | 1916 | T 859 |
DSIR 23/896 | Maybach engine from German airship S.L.II: analysis and strength tests of metal parts | 1916 | T 882 |
DSIR 23/897 | R.A.F. aluminium petrol engine cylinder: heat emission of vibrating iron strips attached to fins | 1916 | T 883 |
DSIR 23/943 | Air-cooled engine cylinder: effect of surface roughness on cooling | 1917 | T 929, 929a |
DSIR 23/968 | Object of tabulating engine data | 1917 | T 954 |
DSIR 23/986 | Water-cooled engines: difficulties experienced in winter in connection with water circulation | 1917 | T 972 |
DSIR 23/1024 | Dissipation of heat from surface of an air-cooled engine when running and at rest | 1917 | T 1010 |
DSIR 23/1051 | Fractured Italian Gnome engine crankshaft: examination | 1917 | T 1037 |
DSIR 23/1085 | Cooling of engines | 1918 | T 1071 |
DSIR 23/1142 | Variation of engine power with height | 1918 | T 1128 |
DSIR 23/1166 | Windage experiments with model of rotary engine B.R.1 | 1918 | T 1152 |
DSIR 23/1167 | Apparatus for measurement in wind tunnel of performance of airscrew or windage torque of rotary engine | 1918 | T 1153 |
DSIR 23/1241 | Best gliding angle in space for aeroplane in a wind with engine shut off | 1918 | T 1227, 1227a |
DSIR 23/1260 | Airscrews designed for S.E.5 aeroplane with 150 H.P. ungeared Hispano-Suiza engine: tests | 1918 | T 1246 |
DSIR 23/1305 | Airscrew, rotary B.R.2 engine, two different types of engine cowling and body of Snipe aeroplane: model experiments | 1919 | T 1291 |
DSIR 23/1331 | Experiments with model of S.E.5 aeroplane and models of several airscrews designed for 150 H.P. ungeared Hispano Suiza engine | 1919 | T 1317, 1317a |
DSIR 23/1433 | Full-scale determination of lift and drag coefficient of biplanes, by means of engine and airscrew performance | 1919 | T 1419 |
DSIR 23/1481 | Comparison of flying qualities of single and twin-engined aeroplanes | 1920 | T 1467 |
DSIR 23/1500 | Installation of Wasp engine in Avro aeroplane | 1920 | T 1486, 1486a |
DSIR 23/1532 | Comparative performance of various airscrews for SE5A aeroplane with Wolseley Viper engine | 1920 | T 1518 |
DSIR 23/1556 | Possible developments of aircraft engines for civil aviation in the next ten years | 1920 | T 1542 |
DSIR 23/1562 | Ricardo experimental engine: notes on research work that could be done at Universities | 1921 | T 1548, 1548a |
DSIR 23/1600 | DH 9 aeroplane No. H 9140 with Handley Page wing and Siddeley Puma 230 H.P. engine: trials | 1921 | T 1586, 1586a |
DSIR 23/1631 | Aerodynamic merits of radial and rotary engines | 1921 | T 1617, 1617a |
DSIR 23/1634 | Full-scale experiments on Handley Page single slotted aerofoil: determination of lift and drag by glides with engine throttled | 1921 | T 1620 |
DSIR 23/1662 | Programme of research on aircraft engines | 1921 | T 1648 |
DSIR 23/1685 | Prevention of fire in single-engined aeroplanes | 1921 | T 1671 |
DSIR 23/1700 | Investigation of engine failures in relation to accidents to aeroplanes | 1922 | T 1686 |
DSIR 23/1719 | Investigation into resistance of twin-engined aeroplanes | 1922 | T 1705 |
DSIR 23/1845 | Power plant reliability and reliability test on German engines | 1923 | T 1831 |
DSIR 23/1847 | Some experiments on airscrews at zero torque, with applications to a helicopter descending with engine off | 1923 | T 1833 |
DSIR 23/1853 | New disposition of engines for twin-engined commercial aeroplane | 1923 | T 1839 |
DSIR 23/1861 | Lift and drag of standard Bristol fighter aeroplane with R.A.F.4d engine | 1923 | T 1847 |
DSIR 23/1893 | Experiments with rudders on two twin-engine aeroplanes | 1923 | T 1879 |
DSIR 23/1965 | Aerodynamical features of proposed multi-engined aeroplane | 1924 | T 1951, 1951a-c |
DSIR 23/1966 | Variation of engine power with height | 1924 | T 1952 |
DSIR 23/1978 | Variation of engine power with height | 1924 | T 1964 |
DSIR 23/2020 | Comparison between air-cooled and water-cooled engines | 1924 | T 2006 |
DSIR 23/2093 | Accidents, forced landings and engine failures | 1925 | T 2079, 2079a |
DSIR 23/2113 | Variable pitch airscrews suitable for service engines: report | 1925 | T 2099, T 2099a |
DSIR 23/2147 | Necessary size of aerodromes for a landing if engine fails at take-off | 1926 | T 2133 |
DSIR 23/2165 | Investigation into action of dopes and detonation in engines | 1925 | T 2151 |
DSIR 23/2241 | Torsional vibration in engines | 1926 | T 2227, 2227a-c |
DSIR 23/2451 | Discussion of law of variation of engine power with height | 1927 | T 2437 |
DSIR 23/2474 | Fire prevention in single-engined aeroplanes | 1927 | T 2460, 2460a |
DSIR 23/2508 | Performance of several combustion chambers designed for aircraft oil engines | 1927 | T 2494 |
DSIR 23/2509 | Effects of fuel and cylinder gas densities on characteristics of fuel sprays for oil engines | 1927 | T 2495 |
DSIR 23/2510 | Factors in design of centrifugal type injection valves for oil engines | 1927 | T 2496 |
DSIR 23/2534 | Determination of horsepower height factor of engines from results of type trials of aeroplanes | 1927 | T 2520 |
DSIR 23/2542 | Bristol `Jupiter' engine: cowling and cooling research | 1927-1928 | T 2528, 2528a-b |
DSIR 23/2581 | Engine researches | 1928 | T 2567 |
DSIR 23/2596 | Proposed forced draught system of cooling aero engines | 1928 | T 2582 |
DSIR 23/2614 | Conference on cooling of air-cooled engines: report | 1928 | T 2600 |
DSIR 23/2619 | Engine Sub-Committees: work on airship engines | 1928 | T 2605 |
DSIR 23/2623 | Cowling for radial air-cooled engine: wind tunnel experiments | 1928 | T 2609 |
DSIR 23/2686 | Method of reducing drag of radial engines by addition of rings of aerofoil section | 1928 | T 2672 |
DSIR 23/2724 | Six-monthly programme of research: suggestions by Society of British Aircraft Constructors for inclusion of items of research into engines | 1928-1929 | T 2710, 2710a-c |
DSIR 23/2732 | Effect of increasing engine power on aircraft performance | 1928 | T 2718 |
DSIR 23/2749 | Magnesium alloys for engine parts | 1929 | T 2735 |
DSIR 23/2810 | Additional external engine cowlings: drag tests | 1929 | T 2796, 2796a-b |
DSIR 23/2833 | Reduction of drag of radial engines by attachment of rings of aerofoil section | 1929 | T 2819 |
DSIR 23/2847 | Effect on performance of restricting an engine to normal r.p.m. at operational height | 1929 | T 2833 |
DSIR 23/2926 | Effect of engine gearing on turning tendency of aircraft | 1929 | T 2912 |
DSIR 23/2956 | Sleeve Valve Panel of Engine Sub-Committee: report | 1930 | T 2942 |
DSIR 23/2964 | H.E.I. Panel of Engine Sub-Committee: report | 1930 | T 2950 |
DSIR 23/2965 | Transmission of vibrations from engine to fuselage of aeroplane | 1930 | T 2951 |
DSIR 23/2968 | Engine and aircraft vibration: conference at Royal Aircraft Establishment, Farnborough | 1930 | T 2954 |
DSIR 23/3000 | Cowling of air-cooled engines: wind tunnel experiments | 1930 | T 2986 |
DSIR 23/3013 | International Research Committee: engine-less flight | 1930 | T 2999 |
DSIR 23/3047 | Use of engine-less gliders or light aeroplanes for obtaining meteorological data | 1930 | T 3033 |
DSIR 23/3107 | Correction to standard atmospheric conditions of performance tests on aircraft fitted with supercharged engines for heights below full throttle height | 1931 | T 3093 |
DSIR 23/3115 | Measurement of performance of Supermarine `S.5' seaplane fitted with ungeared Lion VIIA engine | 1931 | T 3101 |
DSIR 23/3158 | Effect of cowlings and rings on engine cooling | 1931 | T 3144, 3144a-b |
DSIR 23/3215 | Effect of sideslip on performance of multi-engined aircraft | 1932 | T 3201 |
DSIR 23/3252 | Effect of increased carburettor pressure on engine performance at several compression ratios | 1932 | 1 |
DSIR 23/3271 | Lynx engine: tests at high oil temperatures | 1932 | 20 |
DSIR 23/3282 | Thermoelement for exploring temperature distribution over barrel of aero-engine cylinders | 1932 | 31 |
DSIR 23/3300 | Engine Sub-Committee: 64th report | 1932 | 49 |
DSIR 23/3319 | Use of large valve overlap in scavenging a supercharged spark-ignition engine using fuel injection | 1932 | 68 |
DSIR 23/3389 | Air-cooled aircraft engine: tests with petrol and butane | 1932 | 138 |
DSIR 23/3398 | Engine Sub-Committee: 65th report | 1932 | 147 |
DSIR 23/3411 | Torsiograph investigations on radial engine with and without spring-hub, with some reference to damping | 1932 | 160 |
DSIR 23/3431 | Effect on aeroplane performance of factors that must be considered in applying low-drag cowling to radial engines | 1932 | 180 |
DSIR 23/3439 | Compression-ignition engines: tests of several fuels | 1932 | 188 |
DSIR 23/3447 | Compound engine: report | 1932 | 196 |
DSIR 23/3454 | Hart P.V. aircraft fitted with Panther engine: spinning tests | 1931 | 203 |
DSIR 23/3459 | Lubrication of aircraft engines | 1932 | 208 |
DSIR 23/3466 | List of papers circulated to Engine Sub-Committee | 1932 | 215 |
DSIR 23/3487 | Best basis of reduction of supercharged engines from flight tests | 1932 | 236, 236a |
DSIR 23/3488 | High speed compression ignition engine: investigation of processes of combustion. in cylinder | 1932 | 237 |
DSIR 23/3498 | Possible tests of certain engines to destruction | 1932 | 247 |
DSIR 23/3520 | Effect of humidity on engine performance | 1932 | 269 |
DSIR 23/3528 | Engine Sub-Committee: 66th report | 1932 | 277 |
DSIR 23/3560 | Alcohol-petrol blended fuel: engine tests | 1932 | 309 |
DSIR 23/3564 | Effect of humidity on engine power at altitude | 1932 | 313 |
DSIR 23/3575 | High speed compression ignition engine: fuel vapourisation and effect on combustion | 1932 | 324 |
DSIR 23/3590 | Engine Sub-Committee: 67th report | 1932 | 339 |
DSIR 23/3602 | Research engines | 1932 | 351 |
DSIR 23/3606 | Wholly-reconditioned mineral lubricating oil: engine, chemical and physical tests of samples | 1932 | 355 |
DSIR 23/3614 | `R' engines: proposed tests to destruction | 1932 | 363 |
DSIR 23/3638 | Internal combustion engine: work in progress at Manchester University | 1932 | 387 |
DSIR 23/3639 | E.35 engines: progress report on work carried out at Loughborough College | 1932 | 388 |
DSIR 23/3660 | Rolls Royce F.XI engines: torsional vibration characteristics | 1931 | 409 |
DSIR 23/3665 | Leopard `J' engines: torsional vibration | 1931 | 414 |
DSIR 23/3666 | Panther engine: torsional vibration characteristics | 1930 | 415 |
DSIR 23/3667 | Ricardo S.55 engine: investigation of crankshaft strength and resonance characteristics | 1930 | 416 |
DSIR 23/3680 | Short R.6/28 six-engined flying boat: noise measurement | 1932 | 429 |
DSIR 23/3685 | Engines: fading in flight | 1933 | 434 |
DSIR 23/3701 | Nacelle-propeller combinations in various positions with reference to wings: pt II, thick wing, various radial-engine cowlings and tractor propeller | 1933 | 450 |
DSIR 23/3708 | Twelve cylinder Vee aero engine: torsional resonance characteristics | 1933 | 457 |
DSIR 23/3710 | 4/9 - scale model engine nacelles with various cowlings: drag tests | 1933 | 459 |
DSIR 23/3733 | Internal combustion engines: rates of fuel discharge as affected by design of fuel-injection systems | 1933 | 482 |
DSIR 23/3738 | Engine Sub-Committee: 68th report | 1933 | 487 |
DSIR 23/3758 | Oil engine injection problems: investigations at King's College, London | 1933 | 507 |
DSIR 23/3774 | Compression-ignition engine: influence of several factors on ignition lag | 1933 | 523 |
DSIR 23/3775 | Compression-ignition engine with pre-combustion chamber: effect of clearance distribution on performance | 1933 | 524 |
DSIR 23/3776 | Compression-ignition engine with pre-combustion chamber: effect of connecting passage diameter on performance | 1933 | 525 |
DSIR 23/3789 | Two-stroke cycle compression ignition aircraft engine: design and performance estimates | 1933 | 538 |
DSIR 23/3798 | Imperial Airways engines: fuel consumption in summer and winter | 1933 | 547 |
DSIR 23/3803 | Wind tunnel investigation of forced air-cooling for aero-engines | 1933 | 552 |
DSIR 23/3823 | `R' engine components: strengths | 1933 | 572 |
DSIR 23/3824 | Reduction of performance to standard atmosphere for aircraft with supercharged engines | 1932 | 573 |
DSIR 23/3843 | Engine Sub-Committee: 69th report | 1933 | 592 |
DSIR 23/3844 | Economic cooling of engines | 1933 | 593, 593a |
DSIR 23/3860 | Boulton and Paul 3-engined night bomber: suggested programme of tests in connection with prevention of servo rudder flutter | 1933 | 609 |
DSIR 23/3892 | Engine Sub-Committee: air measurements | 1933 | 641 |
DSIR 23/3907 | List of papers circulated to Engine Sub-Committee | 1933 | 656 |
DSIR 23/3946 | Junkers Jumo 5C1 engine | 1933 | 695 |
DSIR 23/3950 | Effect of air intake temperatures on petrol engine performance | 1933 | 699 |
DSIR 23/3955 | Analysis of cylinder gases in petrol engine at end of compression stroke and beginning of expansion stroke | 1933 | 704 |
DSIR 23/3959 | Root's type aircraft engine supercharger: bench and flight tests | 1933 | 708 |
DSIR 23/3997 | `R' engine components: strength | 1933 | 746 |
DSIR 23/3998 | Engine Sub-Committee: 70th report | 1933 | 747 |
DSIR 23/4010 | Water-cooled aircraft engine: tests with petrol and butane under altitude conditions | 1933 | 759 |
DSIR 23/4039 | Mufflers for aeroplane engines | 1933 | 788 |
DSIR 23/4078 | Kestrel II S engine: bench tests under altitude conditions | 1933 | 827 |
DSIR 23/4081 | Internal combustion engine ignition | 1933 | 830 |
DSIR 23/4098 | Jupiter VII engine: bench tests under artificial altitude conditions | 1931 | 847 |
DSIR 23/4108 | Alcohol, acetone etc. in air-cooled engine | 1933 | 857 |
DSIR 23/4116 | Engine Sub-Committee: 71st report | 1933 | 865 |
DSIR 23/4119 | Mercury and Pegasus engines: beating vibration experienced | 1933 | 868 |
DSIR 23/4146 | Armstrong Whitworth four-engined monoplane: tests | 1933 | 895, 895a-c |
DSIR 23/4165 | Engine Sub-Committee: 72nd report | 1933 | 914 |
DSIR 23/4175 | Fuel-injection spark-ignition engine using a hydrogenated safety fuel | 1933 | 924 |
DSIR 23/4185 | Compression-ignition engine: increasing air charge and scavenging clearance volume | 1933 | 934 |
DSIR 23/4244 | Coil ignition for aero engines: discussion at Royal Aircraft Factory, 5th October | 1933 | 993 |
DSIR 23/4258 | Two cycle compression-ignition engine E.40: report on fifty hour endurance test | 1933 | 1007 |
DSIR 23/4263 | Light products from lubricating oil and engine operation | 1934 | 1012 |
DSIR 23/4277 | Estimation of combustion products from cylinder of petrol engine | 1934 | 1026 |
DSIR 23/4338 | Engine Sub-Committee: 74th report | 1934 | 1087 |
DSIR 23/4349 | Aero-engine lubricating oil | 1934 | 1098 |
DSIR 23/4367 | Three-engined night bomber: full-scale investigation of rudder oscillation | 1934 | 1116 |
DSIR 23/4372 | Matters raised at meeting with engine designers on 6th March | 1934 | 1121 |
DSIR 23/4379 | Operation of air-cooled engines on weak mixtures | 1934 | 1128 |
DSIR 23/4419 | Multi-cylinder water-cooled aero-engine: direct petrol injection experiments | 1934 | 1168 |
DSIR 23/4428 | Direct petrol injection: discussion with engine designers, 6th March | 1934 | 1177 |
DSIR 23/4429 | Lubrication: discussion with engine designers, 6th March | 1934 | 1178 |
DSIR 23/4432 | Engine Sub-Committee: terms of reference and membership of Panels | 1934 | 1181 |
DSIR 23/4433 | Relation of hydrogen and methane to carbon monoxide in exhaust gases from internal-combustion engines | 1934 | 1182 |
DSIR 23/4434 | Comparison of several methods of measuring ignition lag in compression-ignition engine | 1934 | 1183 |
DSIR 23/4446 | Abstract of correspondence on engine matters raised at meeting with Society of British Aircraft Constructors, 9th January | 1934 | 1195 |
DSIR 23/4462 | Corrosion of roller bearings in aircraft engines | 1934 | 1211 |
DSIR 23/4520 | Plant for testing aero-engines under high-altitude conditions at Isotta-Fraschini motor car factory: extract from Italian press | 1934 | 1269 |
DSIR 23/4523 | E.35 engine with pump injection into induction pipe: petrol injection tests | 1934 | 1272 |
DSIR 23/4529 | Engine Sub-Committee: 75th report | 1934 | 1278 |
DSIR 23/4579 | Range of Fury aeroplane and fuel consumption of fully supercharged Kestrel engine with flame traps, under varying conditions of mixture strength and ignition advance | 1934 | 1328 |
DSIR 23/4604 | Cooling of air-jacketed engine: wind tunnel investigation | 1934 | 1353 |
DSIR 23/4605 | Comparison of variable and fixed pitch air-screws on long range aeroplane with compression ignition engine | 1934 | 1354 |
DSIR 23/4609 | List of papers circulated to Engine Sub-Committee | 1934 | 1358 |
DSIR 23/4624 | Rapier engine: wind tunnel tests of cowlings | 1934 | 1373 |
DSIR 23/4644 | Drag of engine nacelle | 1934 | 1393 |
DSIR 23/4653 | Engine performance at weak mixtures | 1934 | 1402 |
DSIR 23/4654 | Horsley aeroplanes: investigation of fading of Condor III engines | 1934 | 1403 |
DSIR 23/4704 | Saro Cloud aeroplane with radial engines: wind tunnel tests | 1934 | 1453 |
DSIR 23/4714 | Engine Sub-Committee: 76th report | 1935 | 1463, 1463a |
DSIR 23/4715 | Hart aeroplane with Kestrel I.B. engine: evaporative cooling tests | 1934 | 1464 |
DSIR 23/4724 | Infra-red radiation from explosions in sparkignition engine | 1934 | 1473 |
DSIR 23/4763 | Use of mixtures of gasoline with ethyl and isopropyl alcohols in internal combustion engines: experiments | 1934 | 1512 |
DSIR 23/4769 | Kestrel II S. engine: effect of induction flame dampers under artificial altitude conditions | 1934 | 1518, 1518a |
DSIR 23/4836 | Engine units in large flying-boats | 1934 | 1585 |
DSIR 23/4838 | Air-cooled engine research in 24' tunnel and preliminary model tests: note on proposed programme | 1934 | 1587 |
DSIR 23/4848 | Specification for lubricating oils for aircraft engines | 1935 | 1597 |
DSIR 23/4860 | Damping arising during torsional vibration of engines | 1935 | 1609 |
DSIR 23/4865 | Research engines | 1935 | 1614 |
DSIR 23/4866 | E.40 two-cycle compression ignition engine embodying junkless head and expanding sleeve: 50-hour endurance test | 1935 | 1615 |
DSIR 23/4903 | Long range monoplane with special Lion XI.A. engine: comparison of fixed pitch, two-pitch, three pitch and variable pitch airscrews | 1934 | 1652 |
DSIR 23/4931 | Blackburn civil monoplane: noise in cabin arising from engine out-of-balance forces | 1935 | 1680 |
DSIR 23/4939 | Items suggested by Society of British Aircraft Constructors Technical Committee for discussion with Engine Sub-committee, 2nd April | 1935 | 1688 |
DSIR 23/4951 | Engine Sub-Committee: 77th report | 1935 | 1700 |
DSIR 23/4957 | Kestrel V engine in `Audox aeroplane: coil ignition interference experiments | 1935 | 1706 |
DSIR 23/4968 | Kestrel II.S. engine: measurement of power under artificial altitude conditions over comprehensive range of induction pipe pressures | 1935 | 1717 |
DSIR 23/4984 | Aircraft engine performance with 100 octane fuel | 1935 | 1733 |
DSIR 23/5033 | Engine Sub-Committee: notes on minutes of 92nd meeting | 1935 | 1782 |
DSIR 23/5038 | Spark-ignition and compression-ignition 2-stroke-cycle engine: description and test results | 1935 | 1787 |
DSIR 23/5039 | Prechamber compression-ignition engine: effect of combustion-chamber shape on performance | 1935 | 1788 |
DSIR 23/5040 | Single-cylinder compression-ignition engine with a displacer piston: performance tests | 1935 | 1789 |
DSIR 23/5052 | Condor compression ignition engine: flight tests | 1935 | 1801 |
DSIR 23/5077 | Comments on preliminary draft of new specification for lubricating oils for aircraft engines | 1935 | 1826, 1826a-c |
DSIR 23/5078 | E.44 sleeve valve two-cycle engine: scavenging efficiency experiments | 1935 | 1827 |
DSIR 23/5092 | Engine Sub-Committee: 78th report | 1935 | 1841 |
DSIR 23/5094 | Completion of petrol-injection research on B.60 engine | 1935 | 1843 |
DSIR 23/5115 | Method of inducing cooling air to flow over rear of engine cylinder | 1935 | 1864, 1864a |
DSIR 23/5117 | Lubricating oils for aircraft engines: 2nd draft specification | 1935 | 1866 |
DSIR 23/5123 | Fully-supercharged Kestrel engine in Hart aeroplane: evaporative cooling tests | 1935 | 1872 |
DSIR 23/5129 | Kestrel V engine: coil ignition experiments | 1935 | 1878 |
DSIR 23/5177 | Cooling of aircraft engines with special reference to ethylene glycol radiators enclosed in ducts | 1935 | 1926 |
DSIR 23/5179 | Examination of torsional vibration characteristics of direct drive, two-throw radial engine | 1935 | 1928 |
DSIR 23/5188 | Transverse vibration of Pegasus II M.3 engine on aerodrome test bed | 1935 | 1937 |
DSIR 23/5194 | Ethylene glycol coolant in Kestrel engines: flight tests | 1935 | 1943 |
DSIR 23/5212 | Handley Page aeroplane G.4/31 with Pegasus III M.S. engine: handling trials | 1935 | 1961 |
DSIR 23/5223 | Mercury VI.S. engine: week mixture tests | 1935 | 1972 |
DSIR 23/5225 | Engine research and development: resumé of principal points raised at Aircraft Conference | 1935 | 1974 |
DSIR 23/5258 | Engine Sub-Committee: 79th report | 1935 | 2007 |
DSIR 23/5279 | Aircraft engine lubricating oils: proposed new specification | 1935 | 2028 |
DSIR 23/5282 | Mercury VIS engine: fuel correlation experiments | 1935 | 2031 |
DSIR 23/5283 | Whirling of radial engines on their mountings: mathematical analysis | 1935 | 2032 |
DSIR 23/5286 | Current position and prospects of two-stroke compression ignition engine | 1935 | 2035 |
DSIR 23/5288 | Cooling drag of cowled radial engine | 1935 | 2037 |
DSIR 23/5300 | Subjects to be discussed at meeting with Society of British Aircraft Constructors Engine Technical Committee, 29th October | 1935 | 2049 |
DSIR 23/5302 | Combined fatigue stresses: suggested programme of research, with special reference to design requirements of aero-engine crankshafts | 1935 | 2051, 2051a |
DSIR 23/5306 | Draco petrol injection engine | 1935 | 2055 |
DSIR 23/5322 | Saro Cloud seaplane with Rapier engines: wind tunnel tests | 1934 | 2071 |
DSIR 23/5329 | Saro Cloud seaplane with Rapier engines: improvement due to fitting continuous slat across centre portion of wing under engine nacelles | 1935 | 2078 |
DSIR 23/5374 | Engine Sub-Committee: 80th report | 1935 | 2123 |
DSIR 23/5381 | Torsional vibration of `R' (Schneider Trophy) 1931 series engine | 1935 | 2130 |
DSIR 23/5393 | Effect on drag of air leaks in air-cooled engine installations | 1935 | 2142 |
DSIR 23/5414 | Revised harmonic analysis of torque curves of single cylinder electric ignition engine | 1935 | 2163 |
DSIR 23/5441 | High-power two-cycle engine for special purpose machines | 1936 | 2190 |
DSIR 23/5500 | Attenuation characteristics of some aero-engine exhaust silencers | 1936 | 2249 |
DSIR 23/5502 | Relative performance of two-stroke and four-stroke petrol engines | 1936 | 2251 |
DSIR 23/5511 | Engines of specially high power | 1936 | 2260 |
DSIR 23/5557 | Light-alloys: programme of research suggested by Engine Technical Committee | 1936 | 2306 |
DSIR 23/5564 | E.25 single-cylinder high pressure engine: super-charging experiments | 1936 | 2313 |
DSIR 23/5570 | Engine Sub-Committee: 81st report | 1936 | 2319 |
DSIR 23/5602 | Pitching moments of 4-engined monoplane with airscrews running | 1936 | 2351 |
DSIR 23/5614 | Proportion of heat of fuel rejected to pistons in various Napier engines | 1936 | 2363 |
DSIR 23/5620 | Types of engine failure causing forced landings | 1936 | 2369 |
DSIR 23/5621 | Limiting outputs of existing engines at low altitudes | 1936 | 2370 |
DSIR 23/5690 | Hydrogen as an auxiliary fuel in compression ignition engines | 1936 | 2439 |
DSIR 23/5716 | Highly boosted C.I. engine | 1936 | 2465 |
DSIR 23/5731 | Combustion engine temperatures by the sodium line-reversal method | 1936 | 2480 |
DSIR 23/5734 | Experiments on E.25 C.I. supercharged engine | 1936 | 2483 |
DSIR 23/5737 | Examination of torsional vibration characteristics of a geared single-throw radial engine | 1936 | 2486 |
DSIR 23/5752 | Engine Sub-Committee: cooling characteristics of a 2-row radial engine | 1936 | 2501 |
DSIR 23/5764 | Engine Sub-Committee: 82nd report | 1936 | 2513 |
DSIR 23/5777 | Radial engine in the 24' tunnel: cowling tests | 1936 | 2526 |
DSIR 23/5781 | Radial air cooled engine in 24' tunnel: cowling tests | 1936 | 2530 |
DSIR 23/5789 | British Aircraft and Engine Constructors | 1936 | 2538 |
DSIR 23/5793 | List of papers circulated to Engine Sub-Sub-Committee | 1936 | 2542 |
DSIR 23/5805 | Analysis of the drag of a nacelle for a radial engine | 1936 | 2554 |
DSIR 23/5812 | Torsional vibration calculations for Goshawk engine | 1936 | 2561, 2561a |
DSIR 23/5824 | Combustion process in the C.I. engine | 1936 | 2573 |
DSIR 23/5825 | C.I. engine with various fuels and dopes: experiments | 1936 | 2574 |
DSIR 23/5829 | Compression ignition engine research | 1936 | 2578 |
DSIR 23/5831 | Perseus IA engine: tests with vaporised fuel | 1936 | 2580, 2580a |
DSIR 23/5833 | 1/5-scale cowled nacelle suitable for baffled radial engines: tests | 1936 | 2582 |
DSIR 23/5841 | Radial engine in the 24' wind tunnel: cowling tests | 1936 | 2590 |
DSIR 23/5854 | Comparative performance of supercharged single cylinder air-cooled engine using normal carburation and fuel injection, and effect of valve overlap | 1936 | 2603 |
DSIR 23/5871 | E.25 C.I. supercharged engine: experiments | 1936 | 2620 |
DSIR 23/5889 | Engine Sub-Committee: 83rd report | 1936 | 2638 |
DSIR 23/5893 | Methane as an engine fuel | 1936 | 2642 |
DSIR 23/5894 | Jupiter VIIIF engine: tests with petrol and butane | 1936 | 2643 |
DSIR 23/5919 | Effect of extreme slipstream on twin-engined monoplane with split or slotted flaps | 1936 | 2668 |
DSIR 23/5920 | Engine Sub-Committee: 84th report | 1936 | 2669 |
DSIR 23/5922 | Methane as an engine fuel | 1936 | 2671 |
DSIR 23/5923 | Use of methane in I.C. engine | 1936 | 2672 |
DSIR 23/5983 | Kestrel engine with pressure-fed carburettor: flight tests | 1936 | 2732 |
DSIR 23/5984 | Engine Sub-Committee: 85th report | 1936 | 2733 |
DSIR 23/6102 | Design and performance possibilities of Royal Aircraft Establishment variable compression engine | 1936 | 2851 |
DSIR 23/6106 | Flat turning of twin-engined machines with one engine cut out | 1937 | 2855 |
DSIR 23/6129 | Installation of a Dagger engine nacelle on a wing | 1936 | 2878 |
DSIR 23/6130 | Review of some cathode ray oscillograph engine indicators | 1937 | 2879 |
DSIR 23/6140 | Extracts of engine matters from reciprocal questionnaire and answers on aeronautical development in U.S.A. | 1937 | 2889 |
DSIR 23/6143 | Indicators for high-speed internal combustion engines | 1937 | 2892 |
DSIR 23/6144 | Engine Sub-Committee: 86th report | 1937 | 2893 |
DSIR 23/6159 | Lateral stability of a single engined high wing monoplane with airscrew running: yawing moments due to sideslip and rudder power | 1937 | 2908 |
DSIR 23/6166 | Heinkel H,e 70 aeroplane with Rolls Royce Kestrel XVI engine: performance tests | 1937 | 2915 |
DSIR 23/6190 | Pressure over a long chord cowl for a radial engine | 1937 | 2939 |
DSIR 23/6203 | 1/5 scale D.H.91 engine nacelle: wind tunnel tests | 1937 | 2952 |
DSIR 23/6212 | Effect of extreme slipstream on a single-engine monoplane with split or slotted flaps: wind tunnel tests | 1937 | 2961 |
DSIR 23/6220 | Bristol twin-engined, single-seater fighter aeroplane: model wind tunnel tests | 1937 | 2969 |
DSIR 23/6230 | Effect of several factors on cooling of a radial engine in flight | 1937 | 2979 |
DSIR 23/6244 | Landing with engine on | 1937 | 2993 |
DSIR 23/6255 | Engine Sub-Committee: 87th report | 1937 | 3004 |
DSIR 23/6267 | Types of electrical pick-up units suitable for engine indicators and detonation meters | 1937 | 3016 |
DSIR 23/6268 | High-speed engine indicators | 1937 | 3017 |
DSIR 23/6273 | Vibration in engine structures | 1937 | 3022 |
DSIR 23/6302 | Prechamber compression-ignition engine performance | 1937 | 3051 |
DSIR 23/6308 | Boosted performance of compression-ignition engine with displacer piston | 1937 | 3057 |
DSIR 23/6309 | Influence of fuel-oil temperature on combustion in a prechamber compression engine | 1937 | 3058 |
DSIR 23/6310 | Friction of compression-ignition engines | 1937 | 3059 |
DSIR 23/6311 | Measurements of fuel distribution within sprays for fuel-injection engines | 1937 | 3060 |
DSIR 23/6314 | Performance of air-cooled engine cylinders using blower cooling | 1937 | 3063 |
DSIR 23/6320 | Engine indicators: development at Proefstation `Delft' | 1937 | 3069 |
DSIR 23/6350 | Engine Sub-Committee: 88th report | 1937 | 3099 |
DSIR 23/6367 | Prevention of snow and ice in intakes and induction systems of engines | 1937 | 3116 |
DSIR 23/6386 | Combustion process in explosion engines | 1936 | 3135 |
DSIR 23/6395 | Fuel spray and flame formation in compression-ignition engine employing air flow | 1937 | 3144 |
DSIR 23/6400 | Engines: comparison tests | 1937 | 3149 |
DSIR 23/6412 | Straight flight of twin-engined aircraft with one engine stopped | 1937 | 3161, 3161a |
DSIR 23/6422 | Proposed installation of aircooled engine inside a wing: model tests | 1937 | 3171 |
DSIR 23/6433 | Tests made with Royal Aircraft Establishment detonation unit and meter at works of engine manufacturers | 1937 | 3182 |
DSIR 23/6464 | Preliminary study of flame propagation in a spark-ignition engine | 1937 | 3213 |
DSIR 23/6478 | Cooling of airplane engines at low air speeds | 1937 | 3227 |
DSIR 23/6480 | Single-row radial engine with several National Advisory Committee for Aeronautics cowling: cooling tests | 1937 | 3229 |
DSIR 23/6487 | Nitrogen oxides in internal combustion engine gases | 1937 | 3236 |
DSIR 23/6504 | Injection systems phenomena of high speed diesel engines | 1937 | 3253 |
DSIR 23/6506 | Engine Sub-Committee: 89th report | 1937 | 3255 |
DSIR 23/6533 | Design of aero-engine super-chargers | 1937 | 3282, 3282a |
DSIR 23/6542 | Propellers for aircraft engines of high power output | 1937 | 3291 |
DSIR 23/6556 | Stability of aviation oils: engine and laboratory tests | 1937 | 3305 |
DSIR 23/6570 | Gloster Hele-Shaw variable pitch airscrew for Kestrel II.S. engine: performance and endurance flight tests | 1937 | 3319 |
DSIR 23/6571 | Standardisation of pitot-static head position on single engined monoplanes | 1937 | 3320, 3320a |
DSIR 23/6573 | Selections of oils for high-output aircraft engines | 1937 | 3322 |
DSIR 23/6591 | Actual values of static mean stress to be employed in research into combined fatigue stresses with special reference to design requirements of aero-engine crankshafts | 1938 | 3340 |
DSIR 23/6592 | Possibilities of utilising increased engine torque at take-off: summary of discussion by Engine Sub-Committee | 1938 | 3341 |
DSIR 23/6607 | Light alloys for use in aero engines: recent discussion with Bristol Aeroplane Company and Rolls Royce Limited | 1938 | 3356 |
DSIR 23/6631 | Effect of air-entry angle on performance of a two-stroke-cycle compression-ignition engine | 1938 | 3380, 3380a |
DSIR 23/6655 | Engine torque indicator: flight tests | 1938 | 3404 |
DSIR 23/6656 | Compression-ignition engine performance at altitudes and at various air pressures and temperatures | 1938 | 3405 |
DSIR 23/6669 | Engine Sub-Committee: 90th report | 1938 | 3418 |
DSIR 23/6689 | Installation of engine nacelle on a wing | 1938 | 3438 |
DSIR 23/6706 | Tiger VI engine: cooling and cowling tests in 24' tunnel | 1937 | 3455 |
DSIR 23/6732 | Engine Sub-Committee: 91st report | 1938 | 3481 |
DSIR 23/6737 | Suppression of detonation in an engine by means of stream | 1938 | 3486 |
DSIR 23/6749 | Air-cooled engine cylinders: heat transfer processes | 1938 | 3498 |
DSIR 23/6753 | Lubricating oils before and after subjection to single-cylinder engine tests: laboratory tests | 1938 | 3502 |
DSIR 23/6766 | Diesel as a high output engine for aircraft | 1938 | 3515 |
DSIR 23/6779 | Society for British Aircraft Constructors: subjects for discussion with Engine Sub-Committee, 26th May | 1938 | 3528 |
DSIR 23/6804 | Engine Sub-Committee: 92nd report | 1938 | 3553 |
DSIR 23/6805 | Engine Sub-Committee: subjects for discussion with Society for British Aircraft Constructors, 26th May | 1938 | 3554 |
DSIR 23/6815 | Problem of ring-sticking in aviation engines | 1938 | 3564 |
DSIR 23/6825 | Review of wind tunnel tests on typical engine nacelle installations | 1938 | 3574, 3574a |
DSIR 23/6843 | Twin-engined high wing monoplanes: wind tunnel tests on position error | 1938 | 3592 |
DSIR 23/6854 | Twin-engined monoplane with airscrews running: longitudinal stability | 1938 | 3603, 3603a |
DSIR 23/6869 | Engine Sub-Committee: 93rd report | 1938 | 3618 |
DSIR 23/6879 | Internal combustion engines: gumming of piston rings | 1938 | 3628 |
DSIR 23/6891 | Heinkel HE 70 aeroplane with Rolls Royce Kestrel XVI engine: performance tests | 1938 | 3640 |
DSIR 23/6892 | Photographic study of combustion and knock in a spark-ignition engine | 1938 | 3641 |
DSIR 23/6907 | Oxides of nitrogen in internal combustion engines | 1938 | 3656 |
DSIR 23/6912 | Stresses in airscrews during engine acceleration | 1938 | 3661 |
DSIR 23/6928 | Tiger VI engine: cooling and cowling tests in 24' wind tunnel | 1938 | 3677 |
DSIR 23/6933 | Engine performance and knock rating of fuels for high-output aircraft engines | 1938 | 3682 |
DSIR 23/6937 | Generator-operated coil ignition systems, with special reference to 24 cylinder engines | 1938 | 3686 |
DSIR 23/6949 | Engine experiments with methane | 1938 | 3698 |
DSIR 23/6950 | Oxygen injection as means of increasing power of compression ignition engines: preliminary tests on E.18 highly-boosted, low compression engine | 1938 | 3699 |
DSIR 23/6962 | Baffling of radial aircooled engines: model tests | 1938 | 3711 |
DSIR 23/6963 | List of papers circulated to Engine Sub-Committee | 1938 | 3712 |
DSIR 23/6969 | Effect of spark-timing regularity on knock limitations of engine performance | 1938 | 3718 |
DSIR 23/6970 | Fuel consumption of a carburettor engine at various speeds and torques | 1938 | 3719 |
DSIR 23/6973 | Water and water-alcohol injection in a supercharged Jaguar engine | 1938 | 3722 |
DSIR 23/6978 | Engine Sub-Committee: 94th report | 1938 | 3727 |
DSIR 23/6992 | Nature and effects on air consumption of fluctuations of pressure in exhaust pipe of a single cylinder, four-stroke, internal-combustion engine | 1938 | 3741 |
DSIR 23/6995 | Stability and Control Sub-Committee: further analysis of experiments on longitudinal stability of a twin-engined monoplane with airscrews running | 1938 | 3744 |
DSIR 23/6999 | Installation of engine nacelle on wing part II: underslung nacelles on cambered wings | 1938 | 3748 |
DSIR 23/7014 | Ricardo two-stroke petrol engine | 1938 | 3763 |
DSIR 23/7018 | Provision of further material for continuation of research into combined fatigue stresses, with special reference to design requirements of aero-engine crankshafts | 1938 | 3767 |
DSIR 23/7060 | Comparison of pusher and tractor airscrews in multi-engine design and possibility of increasing laminar flow area | 1938 | 3809 |
DSIR 23/7087 | Rating aviation fuels in full-scale aircraft engines | 1938 | 3836 |
DSIR 23/7088 | Cylinder cooling and drag of radial engine installations | 1938 | 3837 |
DSIR 23/7098 | Engine Sub-Committee: draft of 95th report | 1939 | 3847 |
DSIR 23/7115 | 4-Stroke C.I. engine: note on research | 1939 | 3864 |
DSIR 23/7119 | Culverin engine: bench tests under artificial altitude conditions | 1938 | 3868 |
DSIR 23/7127 | Sleeve materials: discussion with engine constructors regarding research | 1939 | 3876 |
DSIR 23/7130 | Engine drag | 1939 | 3879 |
DSIR 23/7140 | Kestrel V engine: high power tests using bi-fuel system | 1938 | 3889 |
DSIR 23/7143 | E.40 engine with sleeve-valve and poppet-valve exhaust | 1939 | 3892 |
DSIR 23/7150 | Engine Sub-Committee: draft of 96th report | 1939 | 3899 |
DSIR 23/7164 | Comparison of pusher and tractor airscrews in multi-engine design and possibility of increasing laminar flow area | 1939 | 3913 |
DSIR 23/7187 | Merlin engines: water injection experiments | 1939 | 3938 |
DSIR 23/7192 | Methods of calculation of performance of engines at high altitudes | 1939 | 3943 |
DSIR 23/7195 | Twin-engined aeroplanes: take-off allowing for failure of one engine | 1938 | 3946 |
DSIR 23/7198 | Motor fuels: comparative testing by engine and laboratory test methods | 1939 | 3949 |
DSIR 23/7207 | Engine Sub-Committee: draft of 97th report | 1939 | 3958 |
DSIR 23/7219 | Twin-engined aeroplane: effect of direction of rotatation of airscrews on longitudinal stability | 1939 | 3970 |
DSIR 23/7228 | Full-scale propellers in presence of a radial and liquid-coded engine nacelle: wind tunnel tests | 1939 | 3979 |
DSIR 23/7229 | Air-cooled aeroplane engines: pressure available for ground-cooling in front of cowling | 1939 | 3980 |
DSIR 23/7233 | Increase in engine power | 1939 | 3984 |
DSIR 23/7235 | Twin-engined aircraft: effect of direction of rotation of airscrews on longitudinal stability | 1939 | 3986 |
DSIR 23/7236 | Twin-engined monoplane: effect on longitudinal stability of direction of rotation of airscrews | 1939 | 3987 |
DSIR 23/7283 | Correction of temperatures of air-cooled engine cylinders for variation in engine and cooling conditions | 1939 | 4034 |
DSIR 23/7314 | Present position of E.65 engine research | 1939 | 4065 |
DSIR 23/7320 | Fuel knock rating by U.S. Army Air Corps method with modified C.F.R. engine | 1939 | 4071 |
DSIR 23/7321 | Charging process in high-speed single-cylinder four-stroke engine | 1939 | 4072 |
DSIR 23/7322 | Comparative performance of engines using carburettor, manifold injection and cylinder injection | 1939 | 4073 |
DSIR 23/7327 | Engine Sub-Committee: 98th report | 1939 | 4078 |
DSIR 23/7378 | Altitude behaviour of a precombustion chamber diesel engine: investigation | 1939 | 4129 |
DSIR 23/7414 | Effect of wing engines on natural frequencies and modes of vibration of wings: model experiments | 1939 | 4165, 4165a |
DSIR 23/7436 | Study of air flow in an engine cylinder | 1939 | 4187 |
DSIR 23/7483 | List of papers circulated to Engine Sub-committee | 1939 | 4234 |
DSIR 23/7499 | Influence of directed air flow on combustion in a spark-ignition engine | 1939 | 4250 |
DSIR 23/7500 | Knocking characteristics of fuels in relation to maximum permissible performance of aircraft engines | 1939 | 4251 |
DSIR 23/7517 | Lysander aeroplane: slow speed flying with engine on | 1939 | 4268 |
DSIR 23/7518 | Methane on E.6 variable compression engine: tests | 1939 | 4269 |
DSIR 23/7571 | Engine throttle torque experiments | 1939 | 4322 |
DSIR 23/7634 | Kestrel VI engine using a bi-fuel system: flight tests | 1939 | 4385 |
DSIR 23/7740 | Hercules engine: model tests on cooling under ground running conditions | 1939 | 4491 |
DSIR 23/7783 | Installation of engine nacelle on a wing: effects of fuselage and tractor airscrew | 1939 | 4534 |
DSIR 23/7890 | Use of alcohol in high compression engines | 1916 | I.C.E. 1 |
DSIR 23/7893 | 150-H.P. Le Rhone and 150-H.P. Monosoupape Gnome rotary radial engines: tests | 1916 | I.C.E. 4 |
DSIR 23/7894 | Engine testing | 1916 | I.C.E. 5 |
DSIR 23/7898 | Daimler experimental engine: memorandum | 1916 | I.C.E. 9 |
DSIR 23/7902 | Selection of engines for reproduction | 1917 | I.C.E. 13 |
DSIR 23/7903 | B.H.P. 200-H.P. engine: description prepared from drawings | 1917 | I.C.E. 14 |
DSIR 23/7904 | Hispano-Suiza 200-H.P. engine: description from drawings | 1917 | I.C.E. 15 |
DSIR 23/7905 | B.H.P. 200-H.P. engine: development | 1917 | I.C.E. 16 |
DSIR 23/7906 | Rotary engines: comparison tests | 1917 | I.C.E. 17 |
DSIR 23/7907 | Supercharger B.H.P. engine: development | 1917 | I.C.E. 18 |
DSIR 23/7908 | Hispano-Suiza 200-H.P. engine: tests | 1917 | I.C.E. 19 |
DSIR 23/7909 | Sunbeam aircraft engines: developments | 1917 | I.C.E. 20 |
DSIR 23/7910 | B.H.P. 230-H.P. supercharger engine: development | 1917 | I.C.E. 21 |
DSIR 23/7911 | Sunbeam 200-H.P. and Hispano 200-H.P. engines: comparison tests | 1917 | I.C.E. 22 |
DSIR 23/7912 | Request for considering adopting engines to the use of a supercharger | 1917 | I.C.E. 23 |
DSIR 23/7913 | R.A.F. radial 14-cyl. engine: tests | 1917 | I.C.E. 24 |
DSIR 23/7914 | B.H.P. 200-H.P. engine: tests | 1917 | I.C.E. 25 |
DSIR 23/7915 | Blowers for aeronautical engines: record of progress at the R.A.F. | 1917 | I.C.E. 26 |
DSIR 23/7916 | B.H.P. 200-H.P. engine: 70 hour bench test | 1917 | I.C.E. 27 |
DSIR 23/7917 | B.H.P. 200-H.P. engines: investigation into methods of testing | 1917 | I.C.E. 28 |
DSIR 23/7918 | Hispano-Suiza engine: bench tests carried out in France | 1917 | I.C.E. 29 |
DSIR 23/7920 | Hispano-Suiza, B.H.P. Sunbeam 8-cylinder, and 6-cylinder engines: comparison tests | 1917 | I.C.E. 31 |
DSIR 23/7921 | 8-cylinder and 6-cylinder engines: tests | 1917 | I.C.E. 32 |
DSIR 23/7922 | Hispano-Suiza, B.H.P. Sunbeam 8-cylinder, and 6-cylinder engines: tests | 1917 | I.C.E. 33 |
DSIR 23/7923 | Desirable aeroplane engine | 1917 | I.C.E. 34 |
DSIR 23/7924 | Request for investigation into what type of cylinder and valve gear could be developed into a 200-H.P. engine | 1917 | I.C.E. 35 |
DSIR 23/7925 | Aluminium cylinders for R.A.F. 4 engines | 1917 | I.C.E. 36 |
DSIR 23/7926 | B-12-2a and B-12-2b engines: manufacturing facilities | 1917 | I.C.E. 37 |
DSIR 23/7927 | Outline specifications of new types of engines required by Air Board | 1917 | I.C.E. 38 |
DSIR 23/7929 | Sunbeam engine: conference at Daimler works to discuss aluminium combustion chamber | 1917 | I.C.E. 40 |
DSIR 23/7930 | Test stands for Aero engines | 1917 | I.C.E. 41 |
DSIR 23/7931 | List of suggested matters in connection with aeronautical engines in which research would be of utility | 1917 | I.C.E. 42 |
DSIR 23/7932 | Aero engine: request for discussion on development by Messrs. D. Napier & Son, Ltd. | 1917 | I.C.E. 43 |
DSIR 23/7933 | R.A.F. 4a engine: cylinder tests | 1917 | I.C.E. 44 |
DSIR 23/7934 | R.A.F. 4a engine: suggestions for obviating ill effects from increase of power, and improve reliability generally | 1917 | I.C.E. 45 |
DSIR 23/7935 | Magnetos for super-compression engines | 1917 | I.C.E. 46 |
DSIR 23/7936 | R.A.F. 4a engine: cylinder tests | 1917 | I.C.E. 47 |
DSIR 23/7937 | Case for development of an aero engine designed to work at high altitude and restricted in output near the ground | 1917 | I.C.E. 48 |
DSIR 23/7938 | Engine testing under high altitude conditions | 1917 | I.C.E. 49 |
DSIR 23/7939 | Aero engines: experiments carried out at Lautaret in 1916 | 1917 | I.C.E. 50 |
DSIR 23/7940 | R.A.F. 4d engine: experiments | 1917 | I.C.E. 51, 51a-b |
DSIR 23/7941 | R.A.F. 4d engine: tests at Daimler works | 1917 | I.C.E. 52 |
DSIR 23/7942 | 1st R.A.F. 4d engine: comparative tests of 4a and 4d camshafts | 1917 | I.C.E. 53 |
DSIR 23/7943 | Magnetos for super compression engines at high altitudes | 1917 | I.C.E. 54 |
DSIR 23/7944 | Test stands for aeroplane engines | 1917 | I.C.E. 55 |
DSIR 23/7945 | Suggestions of types of engines required by Air Board | 1917 | I.C.E. 56 |
DSIR 23/7946 | Hispano-Suiza engine: bench tests | 1917 | I.C.E. 57 |
DSIR 23/7947 | Outline specification of new types of engines | 1917 | I.C.E. 58 |
DSIR 23/7948 | Use of chromium steel for valves in Aero engines | 1917 | I.C.E. 59 |
DSIR 23/7950 | Specification laid down for new types of engines required by Air Board | 1917 | I.C.E. 61 |
DSIR 23/7951 | Size of engine suitable for single seater fighter | 1917 | I.C.E. 62 |
DSIR 23/7952 | Design of future engines | 1917 | I.C.E. 63 |
DSIR 23/7953 | Performance of aeroplanes of similar type, with similar engines | 1917 | I.C.E. 64 |
DSIR 23/7954 | Admiralty engine data | 1917 | I.C.E. 65 |
DSIR 23/7956 | Aeroplane engines: test stands | 1917 | I.C.E. 67 |
DSIR 23/7957 | Specified weight of engines in connection with Air Board specification for future engines | 1917 | I.C.E. 68 |
DSIR 23/7958 | B.H.P. 200-H.P. engine cylinder blocks: development | 1917 | I.C.E. 69 |
DSIR 23/7959 | Sunbeam 200-H.P. 8-cylinder engine: progress | 1917 | I.C.E. 70 |
DSIR 23/7960 | Hispano-Suiza 200-H.P. engine: dynamometer tests | 1917 | I.C.E. 71 |
DSIR 23/7961 | Hispano-Suiza 200-H.P. and 150-H.P. engines: tests | 1917 | I.C.E. 72 |
DSIR 23/7962 | Starting of engines in aircraft | 1917 | I.C.E. 73 |
DSIR 23/7963 | Test stands for aeroplane engines | 1917 | I.C.E. 74 |
DSIR 23/7964 | Sunbeam 200-H.P. 8-cylinder engine: tests | 1917 | I.C.E. 75 |
DSIR 23/7965 | Hispano-Suiza 150-H.P. engine: tests | 1917 | I.C.E. 76 |
DSIR 23/7966 | B.H.P. supercharger engine: development | 1917 | I.C.E. 77 |
DSIR 23/7967 | Sunbeam 200-H.P. 8-cylinder engine: development | 1917 | I.C.E. 78 |
DSIR 23/7968 | Cooling fins for aluminium air cooled engines | 1917 | I.C.E. 79 |
DSIR 23/7969 | Cooling of gilled engine cylinders | 1917 | I.C.E. 80 |
DSIR 23/7970 | R.A.F. 4d engine: report after 138 hours running | 1917 | I.C.E. 81 |
DSIR 23/7971 | Carburation of stationary engine at great heights | 1917 | I.C.E. 82 |
DSIR 23/7972 | Spacing of fins for air cooled engines | 1917 | I.C.E. 83 |
DSIR 23/7973 | Sunbeam 200-H.P. 8-cylinder engine No. 3: tests | 1917 | I.C.E. 84 |
DSIR 23/7975 | Air Board requirements for future engines: parts of an engine to be included in its weight | 1917 | I.C.E. 86 |
DSIR 23/7978 | Acetelyne starting of engines: tests | 1917 | I.C.E. 89 |
DSIR 23/7979 | Reduction gears for aeroplane engines | 1917 | I.C.E. 90 |
DSIR 23/7980 | Air cooled engines for military aeroplanes | 1917 | I.C.E. 91 |
DSIR 23/7981 | R.A.F. 4.T.D. engine: cylinder tests to determine best compression ratio | 1917 | I.C.E. 92 |
DSIR 23/7982 | Hispano-Suiza 150-H.P. high compression engine: tests | 1917 | I.C.E. 93 |
DSIR 23/7984 | Effect of method of testing on stresses in crank cases of aero engines, and suggestions for standardisation of test beds | 1917 | I.C.E. 95 |
DSIR 23/7985 | Automatic engine power output regulators for varying altitudes: for use on light engines and blowers | 1917 | I.C.E. 96 |
DSIR 23/7987 | Flexible couplings for engine test beds | 1917 | I.C.E. 98 |
DSIR 23/7988 | Object of tabulating engine data | 1917 | I.C.E. 99 |
DSIR 23/7989 | Power curves of aero engines | 1917 | I.C.E. 100 |
DSIR 23/7990 | Petrol pumps and petrol pump systems for aeroplane engines | 1917 | I.C.E. 101 |
DSIR 23/7991 | Sunbeam Arab 200-H.P. engine No. 9004: running tests | 1917 | I.C.E. 102 |
DSIR 23/7992 | R.A.F. 8.T.2 single cylinder air-cooled engine: temperature distribution tests on aluminium cylinder | 1917 | I.C.E. 103 |
DSIR 23/7995 | Investigation into weight of propellers suitable for any given engine | 1917 | I.C.E. 106 |
DSIR 23/7998 | Steel liners in aluminium air cooled engines | 1917 | I.C.E. 109 |
DSIR 23/7999 | Engine testing | 1917 | I.C.E. 110 |
DSIR 23/8000 | Sunbeam Arab 200-H.P. 8-cylinder engine: final test | 1917 | I.C.E. 111 |
DSIR 23/8001 | Arrangement and details of double hook's joint for test-bed for aeroplane engines | 1917 | I.C.E. 112 |
DSIR 23/8002 | Translation of French method of examination and tests of new aero engines | 1917 | I.C.E. 113 |
DSIR 23/8004 | R.A.F 1a engine: carburation and altitude tests | 1917 | I.C.E. 115 |
DSIR 23/8005 | Fluids for use in the radiators of aero engines | 1917 | I.C.E. 116 |
DSIR 23/8009 | Object of tabulating engine data | 1917 | I.C.E. 120 |
DSIR 23/8010 | Air cooled and water cooled engines for high altitude supercharger work | 1917 | I.C.E. 121 |
DSIR 23/8011 | R.A.F. 4d engine in R.E.8 aeroplane No. A3406: flight tests | 1917 | I.C.E. 122, 122a |
DSIR 23/8012 | French Hispano-Suiza engines: comparison of types | 1917 | I.C.E. 123 |
DSIR 23/8015 | Comparison of effect of engine weight and power on aeroplane performance | 1917 | I.C.E. 126 |
DSIR 23/8017 | Data on German engines | 1917 | I.C.E. 128 |
DSIR 23/8018 | 12-cylinder triple four aero engines: bench tests | 1917 | I.C.E. 129 |
DSIR 23/8020 | Suggested investigation of sparking problems in petrol engine cylinders | 1917 | I.C.E. 131 |
DSIR 23/8028 | Napier triple-four aero engine: Consumption test | 1917 | I.C.E. 139 |
DSIR 23/8029 | Investigation of sparking problems in petrol engine | 1917 | I.C.E. 140 |
DSIR 23/8030 | Relative heat loss from jacket surfaces of multicylinder, water cooled aero engines, when at rest and when in operation | 1917 | I.C.E. 141 |
DSIR 23/8032 | Napier 300-H.P. triple four engine: condition after test | 1917 | I.C.E. 143 |
DSIR 23/8033 | Air cooled and water cooled engines for high altitude supercharger work: tests | 1917 | I.C.E. 144 |
DSIR 23/8035 | R.A.F. 1a engine: carburation and altitude tests | 1917 | I.C.E. 146 |
DSIR 23/8038 | B.R.2. engine: proposed tests | 1917 | I.C.E. 149 |
DSIR 23/8039 | Napier 300-H.P. triple four engine: conclusions arrived at after test | 1917 | I.C.E. 150 |
DSIR 23/8040 | R.A.F. 4.T.D. engine: tests of aluminium air cooled cylinders cast of aluminium alloys B.4, B.18, B19 | 1917 | I.C.E. 151 |
DSIR 23/8041 | Magnetos for 12-cylinder engines | 1917 | I.C.E. 152 |
DSIR 23/8043 | B.R.2. engine No. 1: preliminary tests | 1917 | I.C.E. 154 |
DSIR 23/8046 | Relationship between air temperature and power of petrol engine | 1917 | I.C.E. 157 |
DSIR 23/8047 | B.R.2. engine: tests | 1917 | I.C.E. 158 |
DSIR 23/8048 | Safety spark gap in magnetos for super-compression engines at high altitudes | 1917 | I.C.E. 159 |
DSIR 23/8053 | Siddeley type B.H.P. engine: burning of exhaust valves | 1917 | I.C.E. 164 |
DSIR 23/8055 | Siddeley type B.H.P. engine: burning of exhaust valves | 1917 | I.C.E. 166 |
DSIR 23/8056 | Investigation of effect of change of air density on aero engine power | 1917 | I.C.E. 167 |
DSIR 23/8057 | Variation of engine power with density | 1917 | I.C.E. 168 |
DSIR 23/8058 | Heating of propeller bosses in certain types of engines | 1917 | I.C.E. 169 |
DSIR 23/8059 | Heating of propeller bosses in certain types of engines | 1917 | I.C.E. 170 |
DSIR 23/8062 | Heating of propeller bosses in certain types of engines | 1917 | I.C.E. 173 |
DSIR 23/8063 | Hispano-Suiza 200-H.P. engines: propeller and propeller hub heating | 1917 | I.C.E. 174 |
DSIR 23/8064 | Radiators for water cooled aero engines | 1918 | I.C.E. 175 |
DSIR 23/8065 | B.H.P. and Beardmore engines: bench tests | 1918 | I.C.E. 176 |
DSIR 23/8068 | Colloidal grapjite as an aero engine lubricant | 1918 | I.C.E. 179 |
DSIR 23/8070 | British experimental engines: proposals regarding types to be proceeded with | 1918 | I.C.E. 181 |
DSIR 23/8071 | British experimental engines: present position | 1918 | I.C.E. 182 |
DSIR 23/8073 | Air-cooled engine programme | 1918 | I.C.E. 184 |
DSIR 23/8074 | Torsional vibrations in airscrew and engine shafts of geared engines | 1918 | I.C.E. 185 |
DSIR 23/8076 | British experimental engines: types to be considered | 1918 | I.C.E. 187 |
DSIR 23/8077 | Use of light alloys for aero-engine construction | 1918 | I.C.E. 188 |
DSIR 23/8081 | Steel liners in aluminium air-cooled engines | 1918 | I.C.E. 192 |
DSIR 23/8085 | R.A.F. 3a 230-H.P. water cooled engine: tests to determine effect of change in inlet air temperature, and back pressure, positive and negative | 1918 | I.C.E. 196 |
DSIR 23/8086 | British experimental engines: types to be considered | 1918 | I.C.E. 197 |
DSIR 23/8092 | Case against reduction gears for propeller drive on high powered engines | 1918 | I.C.E. 203 |
DSIR 23/8093 | Daimler 30 - cylinder engine: tests | 1918 | I.C.E. 204 |
DSIR 23/8094 | Expenditure of current and energy required for ignition in an explosion engine | 1918 | I.C.E. 205 |
DSIR 23/8096 | Best rotational speed for airscrew shafts of engines of high power | 1918 | I.C.E. 207 |
DSIR 23/8097 | Air-cooled aircraft engine under construction by Aircraft Manufacturing Co. Ltd. | 1918 | I.C.E. 208 |
DSIR 23/8099 | Piston temperatures in aero-engines | 1918 | I.C.E. 210 |
DSIR 23/8102 | Inverted Vee engine | 1918 | I.C.E. 213 |
DSIR 23/8106 | Natural trend of aero-engine design | 1918 | I.C.E. 217 |
DSIR 23/8107 | Sunbeam Arab engine: official trials | 1918 | I.C.E. 218 |
DSIR 23/8109 | Consideration of the forces acting in radial, rotary and differential engines | 1918 | I.C.E. 220 |
DSIR 23/8110 | Differential type of engine: comparison tests | 1918 | I.C.E. 221 |
DSIR 23/8112 | Similar differential and radial engines: comparison tests | 1918 | I.C.E. 223 |
DSIR 23/8114 | Differential engine: comparison with radial engine | 1918 | I.C.E. 225 |
DSIR 23/8115 | Comparison between radial and differential engines as regards each individual part | 1918 | I.C.E. 226 |
DSIR 23/8117 | Inertia forces in radial and differential engines: Lieut. Col. Barrington's methods applied to C.A.M. engine | 1918 | I.C.E. 228 |
DSIR 23/8118 | R.E.8. aeroplane: installation of Rateau turbo compressor, working in conjunction with R.A.F. 4d engine | 1918 | I.C.E. 229 |
DSIR 23/8119 | Royal Aircraft Establishment: investigation into use of blowers for super-charging aero-engines | 1918 | I.C.E. 230 |
DSIR 23/8120 | Proposed turbo-compressor for a Liberty engine | 1918 | I.C.E. 231 |
DSIR 23/8121 | R.A.F. 4d 12-cylinder Vee engine with aluminium air-cooled cylinders: tests to determine variation in temperature and atmospheric pressure | 1918 | I.C.E. 232 |
DSIR 23/8122 | Dragonfly engine: tests | 1918 | I.C.E. 233 |
DSIR 23/8123 | Investigation into percentage increase of speed obtained with C.A.M. engine as compared with radial engine | 1918 | I.C.E. 234 |
DSIR 23/8131 | Aero-engine lubricants: tests | 1918 | I.C.E. 242 |
DSIR 23/8132 | Aero-engine lubricants: tests | 1918 | I.C.E. 243 |
DSIR 23/8133 | Aero-engine lubricants: tests | 1918 | I.C.E. 244 |
DSIR 23/8137 | Differential engine | 1918 | I.C.E. 248 |
DSIR 23/8148 | Detonation in aero-engine cylinders | 1919 | I.C.E. 259 |
DSIR 23/8160 | Inflamability of engine fuels | 1919 | I.C.E. 271 |
DSIR 23/8161 | Experiments on engines using high flash point fuels | 1919 | I.C.E. 272 |
DSIR 23/8170 | Effect of compression ratio on behaviour of aero-engine at altitude | 1919 | I.C.E. 281 |
DSIR 23/8180 | Engine failures due to defective welding of water-jackets | 1920 | I.C.E. 291 |
DSIR 23/8184 | Fuel tables for aircraft engines | 1920 | I.C.E. 295 |
DSIR 23/8186 | Comparison of torque reactions in various types of engines | 1920 | I.C.E. 297, 297a |
DSIR 23/8193 | Detonation in internal combustion engines | 1920 | I.C.E. 304 |
DSIR 23/8197 | Researches which might be carried out on internal combustion engines at Institutions other than Royal Aircraft Establishment and National Physical Laboratory | 1920 | I.C.E. 308 |
DSIR 23/8198 | Air Ministry Laboratory, engine section: research programme, 1920-1921 | 1920 | I.C.E. 309 |
DSIR 23/8199 | High speed internal combustion engine for research | 1920 | I.C.E. 310 |
DSIR 23/8201 | High compression Benz engine 200-H.P.: variable valve timing tests | 1920 | I.C.E. 312 |
DSIR 23/8207 | Royal Aircraft Establishment: enemy engines tested | 1921 | I.C.E. 318, 318a-b |
DSIR 23/8211 | Provision of internal combustion engine sets to facilitate scientific investigation of aircraft engine problems | 1921 | I.C.E. 322 |
DSIR 23/8212 | Faults experienced in magnetos used in engine experimental departments during 1920 | 1921 | I.C.E. 323 |
DSIR 23/8214 | Air vibrations in engine intake pipes | 1921 | I.C.E. 325 |
DSIR 23/8219 | Testing altitude effiency of internal combustion engines in low pressure chamber at Luftschiffbau Zeppelin G.M.B.H. Friedrichshaven, Germany | 1921 | I.C.E. 330 |
DSIR 23/8220 | High speed engine: development | 1921 | I.C.E. 331 |
DSIR 23/8221 | Adaptation of complete engines to Mr. Ricardo's late-closing inlet valve control | 1921 | I.C.E. 332 |
DSIR 23/8223 | Two curious problems in connection with internal combustion engines | 1921 | I.C.E. 334, 334a |
DSIR 23/8224 | Chart showing effects of fuel on engine performance | 1921 | I.C.E. 335 |
DSIR 23/8226 | Sparking plugs for aircraft engines | 1921 | I.C.E. 337 |
DSIR 23/8230 | New disposition of engines for a twin engine commercial aeroplane | 1921 | I.C.E. 341 |
DSIR 23/8240 | Single cylinder engine 20.T: experimental work at Royal Aircraft Establishment | 1921 | I.C.E. 351, 351a |
DSIR 23/8244 | Hydrogen as fuel for high-speed engines | 1921 | I.C.E. 355 |
DSIR 23/8245 | Engine research at Universities | 1921 | I.C.E. 356 |
DSIR 23/8247 | Design and test of an exhaust collector and silencer for radial engines | 1922 | I.C.E. 358 |
DSIR 23/8253 | Air consumption and B.H.P. of aero-engines | 1922 | I.C.E. 364 |
DSIR 23/8254 | Electrical indicator for high-speed internal combustion engines, and pressure gauge for maximum pressures at Royal Aircraft Establishment | 1922 | I.C.E. 365 |
DSIR 23/8255 | New means of ascertaining mean pressure in a heat engine | 1922 | I.C.E. 366 |
DSIR 23/8259 | Bayern 185-H.P. 6-cylinder engine type B.M.W. IIIA: type tests | 1922 | I.C.E. 370 |
DSIR 23/8262 | Royal Aircraft Establishment single cylinder diesel engine: investigation | 1922 | I.C.E. 373 |
DSIR 23/8267 | Austro Daimler 6-cylinder engine No. 9024: type test | 1922 | I.C.E. 378 |
DSIR 23/8270 | Reliability Panel: type tests of German engines | 1923 | I.C.E. 381 |
DSIR 23/8274 | Distribution and variation of temperature in the cylinder and piston of aircraft engine | 1923 | I.C.E. 385 |
DSIR 23/8279 | Vaporisation of fuels, formation of oil gas and behaviour of oil vapours and gases in diesel engine during combustion | 1923 | I.C.E. 390 |
DSIR 23/8280 | Combustion in diesel engine | 1923 | I.C.E. 391 |
DSIR 23/8281 | Variation in temperature and heat absorption of pistons of internal combustion engines | 1923 | I.C.E. 392 |
DSIR 23/8282 | 4-cylinder car engine: tests using various fuels in conjunction with acetylene gas | 1923 | I.C.E. 393 |
DSIR 23/8288 | Improvement in construction of automobile engines by means of light metal pistons | 1923 | I.C.E. 399, 399a |
DSIR 23/8290 | Phase setting of engine indicators | 1923 | I.C.E. 401 |
DSIR 23/8292 | Power consumption curves for Napier Lion engine with different throttle settings | 1923 | I.C.E. 403, 403a |
DSIR 23/8295 | Power plant reliability and reliability test on German engines | 1923 | I.C.E. 406 |
DSIR 23/8302 | Heat transfer in internal combustion engines | 1923 | I.C.E. 413, 413a |
DSIR 23/8303 | Diesel engine: tests | 1923 | I.C.E. 414 |
DSIR 23/8304 | Variable compression engines for experimental purposes | 1923 | I.C.E. 415 |
DSIR 23/8305 | Possible use of high compression engines at high altitude | 1923 | I.C.E. 416 |
DSIR 23/8306 | Engine development tests | 1923 | I.C.E. 417 |
DSIR 23/8308 | Research work on use of heavy oils for aircraft engines | 1923 | I.C.E. 419 |
DSIR 23/8310 | Engine friction losses: collection of available data | 1923 | I.C.E. 421 |
DSIR 23/8311 | Effect of altitude on engine performance | 1923 | I.C.E. 422, 422a |
DSIR 23/8312 | Possible use of high compression engines at high altitudes | 1923 | I.C.E. 423 |
DSIR 23/8313 | Boosting of a single cylinder Liberty engine working at ground level | 1923 | I.C.E. 424 |
DSIR 23/8314 | Radiation emitted by exploding charge in petrol engine | 1923 | I.C.E. 425 |
DSIR 23/8315 | Benz Rohol two-stage ignition engine | 1923 | I.C.E. 426 |
DSIR 23/8316 | Effect of altitude on engine performance | 1924 | I.C.E. 427 |
DSIR 23/8318 | Calibration of 650-H.P. Rolls Royce Condor series 1a engine | 1923 | I.C.E. 429, 429a |
DSIR 23/8320 | Cams for internal combustion engines | 1923 | I.C.E. 431 |
DSIR 23/8323 | Royal Aircraft Establishment electrical indicator: indicating an aero-engine in flight at various altitudes | 1924 | I.C.E. 434 |
DSIR 23/8324 | Present position of engine research in the programme for 1924-1925 and list of recommendations on which no action has been taken | 1924 | I.C.E. 435 |
DSIR 23/8327 | Improvements in the 4 stroke diesel engine | 1923 | I.C.E. 438 |
DSIR 23/8332 | Investigation into torsional vibration of Lion engine crankshaft | 1924 | I.C.E. 443 |
DSIR 23/8334 | Rolls Royce Falcon III engine: heat distribution experiments | 1924 | I.C.E. 445 |
DSIR 23/8339 | Schedule of standard type and production tests for aircraft engines | 1924 | I.C.E. 450, 450a |
DSIR 23/8340 | Chamber for testing engines under altitude conditions: design | 1924 | I.C.E. 451, 451a |
DSIR 23/8343 | Effect of increasing normal output of aircraft engine | 1924 | I.C.E. 454, 454a |
DSIR 23/8344 | Variation of engine power with height | 1924 | I.C.E. 455 |
DSIR 23/8349 | Internal combustion engines: valve gear rockers | 1924 | I.C.E. 460 |
DSIR 23/8350 | Variation of engine power with height | 1924 | I.C.E. 461 |
DSIR 23/8353 | Bristol Jupiter high compression series IV engine: bi-fuel bench and flight tests | 1924 | I.C.E. 464 |
DSIR 23/8354 | Supercharging of aviation engines | 1924 | I.C.E. 465 |
DSIR 23/8356 | Cylinder head temperature accompanying boiling of water in jackets of a water cooled petrol engine | 1924 | I.C.E. 467 |
DSIR 23/8358 | Effect of reduced intake air pressure on performance of a slow speed solid injection engine | 1924 | I.C.E. 469 |
DSIR 23/8361 | Engine valve springs: compilation and examination of data | 1924 | I.C.E. 472 |
DSIR 23/8362 | Lead: amount present in exhaust gases from engine burning petrol-lead tetra-ethide mixture and in neighbourhood of Laboratory apparatus used for preparing lead tetra-ethide | 1924 | I.C.E. 473 |
DSIR 23/8365 | Engine cooling: evaporative system | 1925 | I.C.E. 476 |
DSIR 23/8366 | Evaporative cooling of aero engines | 1925 | I.C.E. 477 |
DSIR 23/8367 | Supercharging of aircraft engines: conference on 2nd March to discuss questions on scientific aspects | 1925 | I.C.E. 478 |
DSIR 23/8370 | Engine Sub-Committee Panels and the existing membership thereof | 1925 | I.C.E. 481 |
DSIR 23/8374 | Diesel engines: investigation of injection process | 1924 | I.C.E. 485 |
DSIR 23/8375 | Compressor-less diesel engines: processes of injection and combustion | 1924 | I.C.E. 486 |
DSIR 23/8378 | Royal Aircraft Establishment 20.T. single cylinder compression ignition engine Mk. I, bore 8', stroke 11' | 1925 | I.C.E. 489 |
DSIR 23/8383 | Compression ignition engines: starting by means of a gas starter | 1924 | I.C.E. 494 |
DSIR 23/8384 | Variable pitch airscrews suitable for Service engines | 1925 | I.C.E. 495,495a |
DSIR 23/8385 | Investigation into increase in permissible engine speed consequent upon a reduction in weight of reciprocating and rotating masses | 1925 | I.C.E. 496 |
DSIR 23/8387 | Napier Lion engine: tests using lead tetra-ethide as an anti-detonator in aviation spirit | 1925 | I.C.E. 498 |
DSIR 23/8392 | Single sleeve engine: result of tests | 1925 | I.C.E. 503, 503a |
DSIR 23/8394 | Compression ignition engines: statement of research work carried out at various establishments | 1925 | I.C.E. 505 |
DSIR 23/8396 | Blowers for boosting of engines | 1925 | I.C.E. 507 |
DSIR 23/8398 | Compound internal combustion engine | 1925 | I.C.E. 509 |
DSIR 23/8410 | Piston and connecting rod weights and other relative data in modern aircraft engines | 1925 | I.C.E. 521 |
DSIR 23/8411 | Jupiter Mk. IV engine: cylinder temperatures in flight | 1925 | I.C.E. 522 |
DSIR 23/8412 | Torsional vibration in engines: effects of fitting a viscous-friction damper, a flywheel, or a crankshaft-driven supercharger | 1926 | I.C.E. 523, 523a-b |
DSIR 23/8418 | Hydrogen as an auxiliary fuel for a solid injection oil engine | 1926 | I.C.E. 529 |
DSIR 23/8419 | Jupiter series IV engine: comparative possibilities of supercharging and bi-fuel operation | 1926 | I.C.E. 530 |
DSIR 23/8429 | Comparison of possible increment in engine speed for reciprocating and rotating weight reductions | 1926 | I.C.E. 540 |
DSIR 23/8430 | List of papers presented to Engine Sub-committee | 1926 | I.C.E. 541 |
DSIR 23/8441 | Jupiter IV engine: tests using lead tetra ethide as an anti-detonator in aviation spirit | 1926 | I.C.E. 552,552a |
DSIR 23/8442 | Compression ignition engine: improvement of performance by directing flow of the inlet air | 1926 | I.C.E. 553 |
DSIR 23/8448 | Jaguar Mk. IV engine: cylinder temperatures in flight | 1926 | I.C.E. 559 |
DSIR 23/8449 | Lion engine: preliminary development of an oil cooler and automatic oil temperature regulator | 1926 | I.C.E. 560 |
DSIR 23/8452 | Compression ignition engine research | 1926 | I.C.E. 563 |
DSIR 23/8454 | Airship engine development | 1926 | I.C.E. 565,565a |
DSIR 23/8460 | Value of reduced weight of reciprocating and rotating masses on engine performance | 1926 | I.C.E. 571 |
DSIR 23/8462 | Power output and air requirements of a two-stroke cycle engine for aeronautical use | 1927 | I.C.E. 573 |
DSIR 23/8463 | Description of Napier `Lion' racing engine as originally built | 1927 | I.C.E. 574 |
DSIR 23/8464 | Description of Bristol `Mercury' I air-cooled radial engine | 1927 | I.C.E. 575 |
DSIR 23/8466 | Internal combusion engines: investigation into properties of ethylene as a fuel | 1927 | I.C.E. 577 |
DSIR 23/8475 | Airship engine development | 1927 | I.C.E. 586 |
DSIR 23/8477 | Law of variation of engine power with height | 1927 | I.C.E. 588 |
DSIR 23/8478 | Engine Sub-Committee: proposed dates for meetings 1927-1928 | 1927 | I.C.E. 589 |
DSIR 23/8481 | Suggested spring hubbs and dynamometers for aircraft engines | 1927 | I.C.E. 592 |
DSIR 23/8482 | National Advisory Committee for Aeronautics universal test engine: test results | 1927 | I.C.E. 593 |
DSIR 23/8483 | Double acting 2-stroke engines for aircraft | 1927 | I.C.E. 594, 594a-b |
DSIR 23/8485 | Digit engine: trials | 1927 | I.C.E. 596 |
DSIR 23/8489 | Direct measurement of engine power on an aeroplane in flight with hub type dynamometer | 1927 | I.C.E. 600 |
DSIR 23/8492 | Combustion chambers designed for aircraft oil engines: performance | 1927 | I.C.E. 603 |
DSIR 23/8493 | Effects of fuel and cylinder gas densities on characteristics of fuel sprays for oil engines | 1927 | I.C.E. 604 |
DSIR 23/8494 | Factors in design of centrifugal type injection valves for oil engines | 1927 | I.C.E. 605 |
DSIR 23/8499 | Airship engine development | 1927 | I.C.E. 610 |
DSIR 23/8500 | Royal Aircraft Establishment: survey of engine experimental work | 1927 | I.C.E. 611 |
DSIR 23/8505 | Internal combustion engines: motoring losses | 1927 | I.C.E. 616 |
DSIR 23/8506 | Determination of horsepower height factor of engines from results of type trials of aircraft | 1927 | I.C.E. 617 |
DSIR 23/8507 | Internal combustion engines: heat transfer | 1927 | I.C.E. 618 |
DSIR 23/8508 | Friction of aviation engines | 1927 | I.C.E. 619 |
DSIR 23/8511 | Bristol Jupiter engine: cowling and cooling, research | 1927 | I.C.E. 622, 622a |
DSIR 23/8514 | Internal combustion engines: oil gas as a fuel | 1927 | I.C.E. 625 |
DSIR 23/8515 | Gaseous fuels obtained from oil: characteristics and engine performance | 1927 | I.C.E. 626 |
DSIR 23/8516 | Two-cycle compression ignition engine | 1927 | I.C.E. 627 |
DSIR 23/8517 | Combined cycle engine | 1928 | I.C.E. 628, 628a-d |
DSIR 23/8519 | Engine Sub-Committee: proposed dates for meetings 1928-1929 | 1928 | I.C.E. 630 |
DSIR 23/8521 | Engine experimental work at Royal Aircraft Establishment | 1928 | I.C.E. 632 |
DSIR 23/8524 | Comparative performance of an aviation engine at normal and high inlet air temperatures | 1928 | I.C.E. 635 |
DSIR 23/8527 | Fall off in brake horsepower with altitude of naturally aspirated engine considered from the engine point of view | 1927 | I.C.E. 638 |
DSIR 23/8530 | Overcompressed engine using gasoline: relative performance obtained with several methods of control | 1928 | I.C.E. 641 |
DSIR 23/8531 | Engine Sub-Committee and airship engines | 1928 | I.C.E. 642 |
DSIR 23/8534 | Falcon III engine: evaporative cooling | 1928 | I.C.E. 645 |
DSIR 23/8536 | Mercury II, Jupiter VII and Jupiter X engines: performance tests of supercharger | 1928 | I.C.E. 647, 647a |
DSIR 23/8537 | Rusting of engines when using ethyl fluid | 1928 | I.C.E. 648 |
DSIR 23/8538 | Preliminary investigation of super-charging an air-cooled engine in flight | 1928 | I.C.E. 649 |
DSIR 23/8540 | Diesel engine research 1927-1928 | 1928 | I.C.E. 651 |
DSIR 23/8541 | Comparative performance of Roots type aircraft engine superchargers as affected by change in impeller speed and displacement | 1928 | I.C.E. 652 |
DSIR 23/8550 | Investigation of the failure of K.L.G sparking plugs type 476 removed from Napier high speed engine | 1927 | I.C.E. 661 |
DSIR 23/8551 | Failure of Champion sparking plugs type R.11.V removed from Rolls-Royce Falcon XI engine using doped fuel | 1928 | I.C.E. 662 |
DSIR 23/8558 | Rolls Royce Condor V.S. supercharged engine: bench tests | 1928 | I.C.E. 669, 669a-b |
DSIR 23/8560 | Sleeve valve type as a possible line of development for aircraft engines | 1928 | I.C.E. 671 |
DSIR 23/8563 | Airship engines | 1928 | I.C.E. 674 |
DSIR 23/8564 | Exhaust driven supercharged Lion engine: development in flight in a D.H.9a aircraft | 1928 | I.C.E. 675, 675a |
DSIR 23/8568 | Junkers compression ignition engine | 1928 | I.C.E. 679, 679a |
DSIR 23/8571 | Knock rating of fuels for aero engines | 1928 | I.C.E. 682 |
DSIR 23/8572 | Comparison of bouncing pin and variable compression engine methods of comparing detonating values of fuels | 1928 | I.C.E. 683 |
DSIR 23/8573 | Suggestions received from a member of Society of British Aircraft Constructors Ltd. as to items of research work bearing upon aircraft engines which might be included in the research programme for the ensuing six months | 1928 | I.C.E. 684, 684a-c |
DSIR 23/8574 | Effect on aircraft performance of increasing engine power | 1928 | I.C.E. 685 |
DSIR 23/8576 | Engine Sub-Committee: proposed dates for meetings during the year | 1929 | I.C.E. 687 |
DSIR 23/8577 | Performance of a standard aero engine on gaseous fuel | 1928 | I.C.E. 688 |
DSIR 23/8578 | Engine performance obtained from Kerosene/Oil gas mixtures | 1928 | I.C.E. 689 |
DSIR 23/8580 | Lion engine with exhaust driven supercharger of increased dimensions in a D.H.9a aircraft: flight tests | 1928 | I.C.E. 691 |
DSIR 23/8583 | Magnesium alloys for engine parts | 1929 | I.C.E. 694 |
DSIR 23/8587 | Engine knock: some physical aspects | 1929 | I.C.E. 698 |
DSIR 23/8588 | Internal combustion engine: chemical change in fuel/air mixtures during compression, 1st report | 1929 | I.C.E. 699 |
DSIR 23/8590 | Guan aircraft: performance of supercharged Lion V.S. engine | 1928 | I.C.E. 701 |
DSIR 23/8597 | Whirlwind radial air-cooled engine II: drag and cooling with various forms of cowling | 1929 | I.C.E. 708 |
DSIR 23/8599 | High-speed oil engine injection system with an oscilloscope: determination of several spray characteristics | 1928 | I.C.E. 710 |
DSIR 23/8600 | Variation in engine power with altitude determined from measurements in flight with a hub dynamometer | 1929 | I.C.E. 711 |
DSIR 23/8601 | Fawn aircraft: performance of exhaust driven supercharged Lion V.S. engine | 1929 | I.C.E. 712 |
DSIR 23/8602 | Present position of supercharger and supercharged engine research at Royal Aircraft Establishment | 1929 | I.C.E. 713 |
DSIR 23/8606 | E.7 high speed engine | 1929 | I.C.E.717 |
DSIR 23/8612 | Torsional vibration: tornado engine investigations | 1929 | I.C.E. 723 |
DSIR 23/8614 | Proposal for double piston, two cycle compression ignition aero-engine | 1929 | I.C.E. 725 |
DSIR 23/8621 | Supercharged engine fitted with various types of supercharger: comparative performance | 1929 | I.C.E. 732 |
DSIR 23/8623 | Fuel vapour pressures and relation of vapour pressure to preparation of fuel for combustion in fuel injection engine | 1929 | I.C.E. 734 |
DSIR 23/8626 | Investigation of fire risk with various coolants for aircraft engines | 1929 | I.C.E. 737 |
DSIR 23/8627 | Variation of engine power with height | 1929 | I.C.E. 738 |
DSIR 23/8628 | Compression ignition engines: fuel accelerators | 1929 | I.C.E. 739 |
DSIR 23/8630 | Liberty single cylinder engine: ground boosting at specified temperatures | 1929 | I.C.E. 741, 741a |
DSIR 23/8634 | Wright J-5 engine: effect of fuel consumption of cylinder temperatures and performance | 1929 | I.C.E. 745 |
DSIR 23/8638 | Wright J-5 engine: effect of cowling on cylinder temperatures and performance | 1930 | I.C.E. 749 |
DSIR 23/8639 | Engine Sub-Committee: Sleeve Valve Panel | 1930 | I.C.E. 750 |
DSIR 23/8641 | Roots type engine supercharge: tests | 1930 | I.C.E. 752, 752a |
DSIR 23/8646 | Supercharger units for Jaguar engines: characteristics and performance tests | 1927 | I.C.E. 757 |
DSIR 23/8647 | Effect of supercharger capacity on engine and aeroplane performance | 1930 | I.C.E. 758 |
DSIR 23/8652 | Royal Aircraft Establishment automatic boost control on supercharged engines | 1930 | I.C.E. 763 |
DSIR 23/8653 | Transmission of vibrations from the engine to fuselage of an aeroplane | 1930 | I.C.E. 764 |
DSIR 23/8655 | Royal Aircraft Establishment: report on a Conference upon engine and aircraft vibrations held on 30th April | 1930 | I.C.E. 766 |
DSIR 23/8659 | Internal combustion engine: chemical change in fuel/air mixtures during compression, 2nd report | 1929 | I.C.E. 770 |
DSIR 23/8660 | Internal combustion engine: chemical change in fuel/air mixtures during compression, final report | 1930 | I.C.E. 771 |
DSIR 23/8662 | High-speed compression ignition engines: mechanical efficiency | 1930 | I.C.E. 773, 773a |
DSIR 23/8664 | List of papers submitted to Engine Sub-Committee | 1930 | I.C.E. 775 |
DSIR 23/8667 | Diesel engines: compression ratios | 1930 | I.C.E. 778 |
DSIR 23/8668 | Liberty engine: torsional resonance characteristics | 1930 | I.C.E. 779 |
DSIR 23/8669 | Research engines under construction for Air Ministry | 1930 | I.C.E. 780 |
DSIR 23/8670 | Packard air-cooled compression ignition engine | 1930 | I.C.E. 781 |
DSIR 23/8673 | High-speed compression ignition engine using multiple orifice fuel injection nozzles: performance | 1930 | I.C.E. 784 |
DSIR 23/8676 | Diesel engines: limits of compression ratio | 1930 | I.C.E. 787 |
DSIR 23/8677 | E.30 Sleeve valve unit petrol engine: air cooling research | 1930 | I.C.E. 788 |
DSIR 23/8678 | Oxidation characteristics of fuel vapours with regard to engine detonation | 1930 | I.C.E. 789 |
DSIR 23/8683 | Accuracy of comparisons of engine power based on airscrew rotation rate | 1930 | I.C.E. 794 |
DSIR 23/8687 | Compression ignition engine: potential advantages of pre-heating the induction air | 1930 | I.C.E. 798 |
DSIR 23/8690 | Airship compression ignition engines: hydrogen-cum-oil gas as an auxiliary fuel | 1930 | I.C.E. 801 |
DSIR 23/8694 | Relative weight of compression ignition and petrol engines operating at equal maximum pressures | 1931 | I.C.E. 805 |
DSIR 23/8696 | Range of aircraft at heights: flight tests of an aircraft with an air cooled radial engine | 1930 | I.C.E. 807 |
DSIR 23/8699 | Two-cycle compression ignition engines for aircraft | 1931 | I.C.E. 810 |
DSIR 23/8700 | Two-cycle C.I. engine for aircraft | 1931 | I.C.E. 811 |
DSIR 23/8702 | Poppet valve two-cycle compression ignition engine | 1931 | I.C.E. 813 |
DSIR 23/8703 | Petrol and compression ignition engines: comparative weights | 1931 | I.C.E. 814 |
DSIR 23/8704 | E.30 medium speed compression ignition engine: boosting experiments | 1931 | I.C.E. 815,815a |
DSIR 23/8708 | Cooling of engines by liquids at high temperatures | 1930 | I.C.E. 819 |
DSIR 23/8711 | Detonation, spark plug position and engine speed | 1931 | I.C.E. 822 |
DSIR 23/8713 | High speed Poppet valve compression ignition engines | 1931 | I.C.E. 824 |
DSIR 23/8714 | Air-cooled radial engine on weak mixtures and with variable ignition | 1931 | I.C.E. 825 |
DSIR 23/8716 | Ethyl nitrate as a fuel accelerator for compression ignition engines | 1931 | I.C.E. 827 |
DSIR 23/8725 | List of papers submitted to Engine Sub-Committee | 1931 | I.C.E. 836 |
DSIR 23/8726 | Measurement in flight of temperature of air-cooled engine cylinders | 1931 | I.C.E. 837 |
DSIR 23/8727 | Jupiter VIII engine: tests at reduced mixture strengths | 1931 | I.C.E. 838,838a |
DSIR 23/8728 | Air-cooled radial engine on a weak mixture: endurance test | 1931 | I.C.E. 839 |
DSIR 23/8733 | Compression ignition engines: spontaneous ignition temperatures of fuels | 1931 | I.C.E. 844 |
DSIR 23/8735 | Effect of heat interchanges in an internal combustion engine cylinder on volumetric efficiency | 1931 | I.C.E. 846 |
DSIR 23/8738 | Investigation of combustion processes in ignition engines by means of electrical measuring devices | 1931 | I.C.E. 849 |
DSIR 23/8740 | Engine cylinder: flame movement and pressure development | 1931 | I.C.E. 851 |
DSIR 23/8742 | Fuel consumption figures recorded on engine tests at Shoreham | 1931 | I.C.E. 853 |
DSIR 23/8743 | Conversion of Condor engine to compression ignition: preliminary bench tests of complete engine | 1931 | I.C.E. 854 |
DSIR 23/8744 | Compression ignition engine with a pre-combustion chamber having high-velocity air flow: performance | 1932 | I.C.E. 855 |
DSIR 23/8746 | Compression ignition engine: effectiveness of a double-stem injection valve in controlling combustion | 1932 | I.C.E. 857 |
DSIR 23/8748 | Internal combustion engine: electrical measurement of velocity of ignition | 1932 | I.C.E. 859 |
DSIR 23/8750 | Condor single cylinder engine: compression ignition | 1931 | I.C.E. 861 |
DSIR 23/8753 | Compression - ignition engines: hydraulics of fuel injection pumps | 1932 | I.C.E. 864 |
DSIR 23/8754 | Kestrel II engines in Fairey III F. aircraft: development and performance | 1931 | I.C.E. 865,865a |
DSIR 23/8755 | Engine running conditions and the knock rating of fuels | 1932 | I.C.E. 866 |
DSIR 23/8756 | Roughness of engines when running weak | 1932 | I.C.E. 867 |
DSIR 23/8759 | Propeller efficiency as related to gearing of engines | 1918 | Ae Tech 1 |
DSIR 23/9007 | Siskin IIIa aircraft with supercharged jaguar engine: reduction of performance tests | 1926 | Ae Tech 264 |
DSIR 23/9067 | Performances of aircraft with same type engine corrected to standard power | 1927 | Ae Tech 332 |
DSIR 23/9074 | Engine data required for range calculations: work in hand by Engine Dept RAE | 1927 | Ae Tech 340 |
DSIR 23/9079 | Jaguar engine: petrol consumption tests | 1927 | Ae Tech 345 |
DSIR 23/9110 | Interference effects on a streamline body of struts and rings of streamline section, with applications to design of annular exhaust pipes for radial aircraft engines | 1928 | Ae Tech 384 |
DSIR 23/9121 | Drag of exposed cylinders of an air-cooled radial engine | 1928 | Ae Tech 399 |
DSIR 23/9129 | Drag and cooling with various forms of cowling for Whirlwind engine in cabin-fuselage | 1928 | Ae Tech 408 |
DSIR 23/9147 | Relation between National Advisory Committee Aeronautics cowling and ring for reducing the head resistance of air-cooled engines | 1929 | Ae Tech 431 |
DSIR 23/9166 | Effect of wings of single engine aircraft on propulsive efficiency: full scale wind tunnel tests | 1929 | Ae Tech 462 |
DSIR 23/9192 | XF7C-1 aircraft: comparative performance tests using several different engine cowlings | 1930 | Ae Tech 493 |
DSIR 23/9234 | Effect of built-in engine nacelles on air forces of a wing | 1931 | Ae Tech 536 |
DSIR 23/9262 | Engine ring cowlings | 1931 | Ae Tech 564 |
DSIR 23/9265 | Air-cooled engines | 1931 | Ae Tech 567 |
DSIR 23/9294 | Comparative performance of an air-cooled and water-cooled engined aircraft: comparative performance | 1931 | Ae Tech 596 |
DSIR 23/9309 | Resistance effects produced when bodies or engine nacelles are mounted on wings | 1932 | Ae Tech 611 |
DSIR 23/9312 | R.R. 'Kestrel' II engines in Fairey IIIF aircraft: development and performance | 1931-1932 | Ae Tech 614, 614a |
DSIR 23/9323 | Factors that must be considered in applying low-drag cowling to radial engines: effect on aircraft performance | 1932 | Ae Tech 642 |
DSIR 23/9537 | Bristol fighter with Puma engine: lateral control | 1920 | ACC 11 |
DSIR 23/9605 | Record of engine failures | 1922 | G.17.1. |
DSIR 23/9607 | Causes of engine stoppages: collected from service stations | 1922 | G.17.3. |
DSIR 23/9608 | Classification of engine failures | 1922 | G.17.4. |
DSIR 23/9611 | Engine stoppages in the air | 1922 | G.17.7. |
DSIR 23/9612 | Engine failures: unsuccessful flights, R.A.E. reports 1 - 8 | 1922 | G.17.8. |
DSIR 23/9614 | Engine failures: unsuccessful flights. R.A.E. reports 9-18 | 1922 | G.17.10. |
DSIR 23/9617 | Petrol control for 100 H.P. mono engines | 1922 | G.17.13. |
DSIR 23/9618 | Engine failures: unsuccessful flights, R.A.E. reports 18-32 | 1922 | G.17.14. |
DSIR 23/9623 | Record of engine failures 14th Feb - 31st Dec 1922 | 1923 | G.17.19. |
DSIR 23/9624 | Causes of engine failure on flights made by aircraft belonging to British subsidised firms 1st July - 30th Nov 1922 | 1923 | G.17.20. |
DSIR 23/9625 | Engine failures | 1923 | G.17.21. |
DSIR 23/9626 | Analysis of returns of engine failures received from service stations | 1923 | G.17.22. 22a |
DSIR 23/9628 | Engine failures: unsuccessful flights, R.A.E. reports No. 33-44 | 1923 | G.17.24. |
DSIR 23/9630 | Failure or defect in aircraft engine | 1923 | G.17.26. 26a |
DSIR 23/9634 | Engine failures: unsuccessful flights, R.A.E. reports 45-60 | 1923 | G.17.30. |
DSIR 23/9636 | Causes of engine failure on flights made by aircraft used by British subsidised firms 1st Dec 1922 - 30th June 1923 | 1923 | G.17.32. |
DSIR 23/9638 | Defective Napier Lion engine parts returned from Iraq | 1923 | G.17.34. |
DSIR 23/9639 | Seizure of Napier Lion II engines: reports from units in coastal area | 1923 | G.17.35. |
DSIR 23/9640 | Accessibility of engines in relation to engine failures: letter from Air Ministry | 1923 | G.17.36. |
DSIR 23/9847 | Methods for securing engine, carriage and wagon wheels to their axles | 1921 | M.C.37 |
DSIR 23/9989 | Design of engines for long routes on air mail to the east | 1923 | A.T. 1 |
DSIR 23/9990 | Single-engined civil aircraft for European transport | 1923 | A.T. 2 |
DSIR 23/9992 | Three-engined civil aircraft for imperial communications | 1923 | A.T. 4 |
DSIR 23/10007 | Engine throttling | 1923 | A.T.23 |
DSIR 23/10009 | Period between overhaul of engines in use by civil transport firms: letters received by Air Ministry | 1923 | A.T.26 |
DSIR 23/10012 | Multi-engined aircraft | 1924 | A.T.30 |
DSIR 23/10015 | Reliability factor of multi-engined aircraft | 1924 | A.T.33 |
DSIR 23/10017 | Three-engined civil aircraft for imperial communications | 1924 | A.T.38 |
DSIR 23/10018 | Requirements of an air transport engine: conference at Air Ministry 15th May | 1924 | A.T.39 |
DSIR 23/10024 | Jupiter and Lorraine engines: comparative tests | 1924 | A.T.45 |
DSIR 23/10028 | Comparison between air-cooled and water-cooled engines for air transport pt 1 | 1924 | A.T.51 |
DSIR 23/10031 | D.H. 18 Napier Lion engine: petrol consumption trials | 1925 | A.T.58 |
DSIR 23/10034 | Comparison between air-cooled and water-cooled engines for air transport pt 2 | 1925 | A.T.61 |
DSIR 23/10041 | Twin-engined seaplane with Condor engines | 1925 | A.T.71 |
DSIR 23/10049 | Specification of commercial seaplane with three Bristol Jupiter engines | 1926 | A.T.81 |
DSIR 23/10098 | Liability of engines to catch fire at the carburettor | 1919 | F.P.16 |
DSIR 23/10099 | Liability of engines to catch fire at the carburettor | 1919 | F.P.18 |
DSIR 23/10156 | Outbreaks of fire on multi-engined aircraft during past three years | 1921 | F.P.80 |
DSIR 23/10161 | Prevention of fire on single-engined aircraft | 1921 | F.P.85 85a-b |
DSIR 23/10168 | Difference between single and twin-engined aircraft from fire prevention point of view | 1922 | F.P.100 |
DSIR 23/10170 | Prevention of fire in multi-engined aircraft: skeleton report | 1922 | F.P.102 |
DSIR 23/10183 | Petrol systems for twin engined aircraft | 1922 | F.P.115 |
DSIR 23/10189 | Effect of manoeuvres upon petrol supply to an aircraft engine | 1922 | F.P.124 |
DSIR 23/10193 | Boulton & Paul cast aluminium finned manifold on Napier Lion engine: temperature tests | 1922 | F.P.131 |
DSIR 23/10198 | Air intake pipes for Jupitor engines: letter from Director of Research | 1923 | F.P.139 |
DSIR 23/10210 | Engine tests under conditions of reduced density | 1917 | Sc E 7 |
DSIR 23/10216 | Effect of change in petrol-air mixture on power of rotary engines at different altitudes | 1917 | Sc E 13 |
DSIR 23/10235 | Engine and propeller noise on tractor and pusher type aircraft | 1928 | N. 2 |
DSIR 23/10249 | Insulation of engine and of wing bracing in aircraft | 1929 | N.16 |
DSIR 23/10255 | Rubber insulation for engine feet in aircraft | 1929 | N.22 |
DSIR 23/10266 | Spring loaded engine mountings | 1929 | N.33 |
DSIR 23/10287 | Aircraft noise: comparative figures for noises of airscrews, exhausts and engines | 1930 | N.55 |
DSIR 23/10288 | Propeller noise and engine noise and muffling | 1930 | N.56 |
DSIR 23/10297 | Sidestrand aircraft fitted with geared and ungeared engines: noise experiments | 1931 | N.65 |
DSIR 23/10298 | Engine silencing; experiments | 1931 | N.66 |
DSIR 23/10306 | Inspection of mock-up of Supermarine Vickers Rolls-Royce six-engined forty-seater passenger flying boat: visit by Dr A H Davis 22nd October 1931 | 1932 | N.74 |
DSIR 23/10308 | Engine exhaust silencing: experiments | 1932 | N.76 |