UK National Archives at Kew
Ministry of Aviation (AVIA) Propeller Records
Compiled by David Birch - 19 Feb 2014
Citable Reference | Title | Start Date | End Date | References |
AVIA 10/388 | Aircraft propellers and components: programmes and deliveries by De Havilland, Rotol | 1/1/1942 | 31/12/1942 | |
AVIA 10/389 | Aircraft propellers and components: programmes and deliveries by De Havilland, Rotol | 1/1/1942 | 31/12/1942 | |
AVIA 10/390 | Aircraft propellers and components: programmes and deliveries by De Havilland, Rotol | 1/1/1942 | 31/12/1945 | |
AVIA 10/616 | Ministry of Aircraft Production: requirements for machine tools for airframes, undercarriages, propellers, engines, carburettors, magnetos ... | 1/1/1942 | 31/12/1942 | 3/2/2003 |
AVIA 14/106/2 | General arrangement for propeller driven petrol pump | 1/1/1915 | 31/12/1917 | Drawing No. 955W |
AVIA 14/106/3 | Details for propeller driven petrol pump | 1/1/1915 | 31/12/1917 | Drawing No. 956W |
AVIA 14/106/6 | Details for propeller driven pump | 1/1/1915 | 31/12/1917 | Drawing No. 1082W |
AVIA 14/16/43 | Detailed arrangement of fixed Lewis gun mount, firing through propeller | 1/1/1911 | 31/12/1918 | Drg. No. A 9409 |
AVIA 14/17/1/18 | Propeller boss for 70 H.P. Renault engine | 1/1/1911 | 31/12/1918 | Drg. No. A 1227 |
AVIA 14/18/1/47 | Vertical shaft, propeller shaft and bush. Grease cup. Gear box cover. Keys | 1/1/1911 | 31/12/1918 | Drg.No. A 12467 |
AVIA 14/23/1/47 | Mounting and propeller driven air pump | 1/1/1911 | 31/12/1918 | Drg.No. A 10910 |
AVIA 14/24/30 | Details of propeller shaft and coupling | 1/1/1911 | 31/12/1918 | Drg.No. A 1212 |
AVIA 14/24/76 | Details for starting gear and propeller shaft | 1/1/1911 | 31/12/1918 | Drg. No. A 2189 |
AVIA 14/27/11 | Gear shaft and propeller flange details | 1/1/1911 | 31/12/1918 | Drg.No. A 2467 |
AVIA 14/27/6 | Gear shaft and propeller shaft details | 1/1/1911 | 31/12/1918 | Drg.No. A 2422 |
AVIA 14/28/10 | Arrangement of fairing for propeller shafts left hand | 1/1/1911 | 31/12/1918 | Drg.No. A 5411 |
AVIA 14/38/6 | Propeller sleeve and details | 1/1/1911 | 31/12/1918 | Drg.No. A 3258 |
AVIA 14/38/9 | Arrangement and details of propeller shaft | 1/1/1911 | 31/12/1918 | Drg.No. A 3750 |
AVIA 14/48/2 | Details of air pump (propeller driven) | 1/1/1911 | 31/12/1918 | Drg.No. A 3070 |
AVIA 14/48/3 | Arrangement of air pump (propeller driven) | 1/1/1911 | 31/12/1918 | Drg.No. A 3071 |
AVIA 14/50/32 | Specification and details of nose cap for propeller | 1/1/1911 | 31/12/1918 | Drg.No. A 3198 |
AVIA 14/51/51 | Arrangement specification and details of fairing cone and nose cap for propeller | 1/1/1911 | 31/12/1918 | Drg.No. A 3736 |
AVIA 14/51/52 | Details for fairing cone and nose cap for propeller | 1/1/1911 | 31/12/1918 | Drg.No. A 3737 |
AVIA 14/53/8/51 | Two bladed tractor for 200 H.P. Hispano Suiza engine | 1/1/1911 | 31/12/1918 | Drg.No. T 28063 |
AVIA 14/53/8/52 | Two bladed tractor for 150 H.P. Hispano Suiza engine | 1/1/1911 | 31/12/1918 | Drg.No. T 28066 |
AVIA 14/53/8/53 | Four bladed tractor for 200 H.P. Hispano Suiza engine | 1/1/1911 | 31/12/1918 | Drg.No. T 28096 |
AVIA 14/53/8/54 | Four bladed tractor for 200 H.P. Hispano Suiza engine | 1/1/1911 | 31/12/1918 | Drg.No. T 28097 |
AVIA 14/53/8/55 | Two bladed tractor for 200 H.P. Hispano Suiza engine | 1/1/1911 | 31/12/1918 | Drg.No. T 28098 |
AVIA 14/53/9/13 | General arrangement of propeller boss drive for `C.C.' interrupter gear generator | 1/1/1911 | 31/12/1918 | Drg.No. A 11271 |
AVIA 14/53/9/14 | General arrangement of propeller boss drive for `C.C.' interrupter gear generator | 1/1/1911 | 31/12/1918 | Drg.No. A 11278 |
AVIA 14/53/9/15 | Gear wheels for propeller boss and generator, bush for bracket, bracket for oiling cap, nut | 1/1/1911 | 31/12/1918 | Drg.No. A 11279 |
AVIA 14/53/9/17 | Propeller boss drive for Constantinesco gear on Hispano Suiza geared engine | 1/1/1911 | 31/12/1918 | Drg.No. A 11456 |
AVIA 14/53/9/18 | Gear wheels for propeller boss and generator, nut and washer for bracket, adjusting eyebolt, washer | 1/1/1911 | 31/12/1918 | Drg.No. A 11491 |
AVIA 14/53/9/22 | Propeller boss drive for `C.C' gear | 1/1/1911 | 31/12/1918 | Drg.No. A 11511 |
AVIA 14/53/9/24 | Propeller boss for 200 H.P. Hispano Suiza engine and `C.C.' drive | 1/1/1911 | 31/12/1918 | Drg.No. A 11757 |
AVIA 14/53/9/27 | General arrangement of propeller boss drive, C.C. interrupter gear | 1/1/1911 | 31/12/1918 | Drg.No. A 12780 |
AVIA 14/53/9/29 | Bracket for generator, gear wheel on generator, gear wheel on propeller boss | 1/1/1911 | 31/12/1918 | Drg.No. A 13012 |
AVIA 14/53/9/30 | General arrangement of propeller boss drive for `C.G.' interrupter gear | 1/1/1911 | 31/12/1918 | Drg.No. A 13020 |
AVIA 14/66/1 | Details of boss metal propeller | 19/6/1912 | 19/6/1912 | Drawing No.: T 1368 |
AVIA 14/66/2 | Details of blade metal propeller | 18/6/1912 | 18/6/1912 | Drawing No.: T 1369 |
AVIA 14/66/3 | Arrangement and details of propeller boss for thrust-meter | 25/10/1912 | 25/10/1912 | Drawing No.: T 1714 |
AVIA 14/66/4 | 6 bladed metal propeller; details of blade | 16/8/1913 | 16/8/1913 | Drawing No.: T 2702A |
AVIA 14/66/5 | 6 bladed metal propeller; general arrangement | 16/8/1913 | 16/8/1913 | Drawing No.: T 2704 |
AVIA 14/66/7 | Experimental metal propeller; details | 24/6/1914 | 24/6/1914 | Drawing No.: T 4003 |
AVIA 14/73/2 | 4 bladed propeller for 100 H.P. monosoupape Gnome engine | 10/12/1915 | 10/12/1915 | Drawing No. T 7928 |
AVIA 14/79/1 | 2 bladed propeller with 80 H.P. Gnome engine | 22/5/1913 | 22/5/1913 | Drawing No. T 2448 |
AVIA 14/79/2 | 2 bladed propeller with 80 H.P. Gnome engine | 19/12/1913 | 19/12/1913 | Drawing No. T 3277 |
AVIA 14/80/1 | Propeller for aeroplane with 160 H.P. Gnome engine Diag. angle of attack | 27/4/1914 | 27/4/1914 | Drawing No. T 3361 |
AVIA 14/87/11 | General arrangement of variable pitch propeller | 8/9/1920 | 25/9/1920 | Drawing No. T 34553 |
AVIA 14/87/13 | Standard propeller hubs | 19/8/1921 | 30/9/1921 | Drawing No. T 45335 |
AVIA 14/87/14 | Turbine propeller | 29/1/1924 | 4/2/191924 | Drawing No. T 47358 |
AVIA 14/87/16 | Propeller | 19/10/1925 | 2/11/1925 | Drawing No. T 48299 |
AVIA 14/87/2 | Variable pitch propeller boss; weight controlled | 25/4/1918 | 2/12/1919 | Drawing No. T 24222 |
AVIA 15/1949 | ENGINES: Gas Turbine Engine (Code 22/2): Agreement with De Havilland Aircraft Co. and Allis-Chalmers Mfg. ... | 1/1/1943 | 31/12/1945 | SB. 52211 |
AVIA 15/1949 | PURCHASES FROM ABROAD: Equipment (Code 40/3): Agreement with DeHavilland Aircraft Co. and Allis-Chalmers Mfg of ... | 1/1/1943 | 31/12/1945 | SB. 52211 |
AVIA 15/1950 | AIRCRAFT: Design and Development: Fighters and Fighter-Bombers (Code 6/3): Spitfire XIV fighter fitted with contrarotating ... | 1/1/1943 | 31/12/1946 | SB.52225 |
AVIA 15/2032 | AIRCRAFT: Design and Development: Transport, Gliders and Troopcarriers (Code 6/6): Consideration of use of towed ... | 1/1/1944 | 31/12/1944 | SB.56866 |
AVIA 15/2035 | AIRCRAFT EQUIPMENT: General (Code 8/1): Investigation into improved Sound Insulation of Microphones for use in ... | 1/1/1944 | 31/12/1946 | SB.57600 |
AVIA 15/2082 | AIRCRAFT: Design and Development: Transport, Gliders and Troopcarriers (Code 6/6): Consideration of transport aircraft with ... | 1/1/1944 | 31/12/1945 | SB.60042 |
AVIA 15/2082 | ENGINES: Gas Turbine Engine (Code 22/2): Consideration of transport aircraft with turbine-driven propellers | 1/1/1944 | 31/12/1945 | SB 60042 |
AVIA 15/2119 | AIRCRAFT EQUIPMENT: General (Code 8/1): Development of two speed reduction gears and contra rotating propellers; ... | 1/1/1941 | 31/12/1945 | SB.61308 |
AVIA 15/2218 | ENGINES: Research and Development (Code 22/1): Consideration of Long Range I turbine propeller engine project | 1/1/1945 | 31/12/1945 | SB. 65104 |
AVIA 15/2231 | ENGINES: Gas Turbine Engine (Code 22/2): Engine test bed for turbine propeller engine: installations policy | 1/1/1945 | 31/12/1948 | SB 65221 |
AVIA 15/2274 | ENGINES: Gas Turbine Engine (Code 22/2): 250 HP gas turbine propeller engine: Research by Power ... | 1/1/1946 | 31/12/1948 | SB 67179 |
AVIA 15/2568 | AIRCRAFT: GENERAL - Maintenance and Repair (Code 5/7): Repair and maintenance of engines and propellers ... | 1/1/1943 | 31/12/1943 | Prod/Pol/43 |
AVIA 15/2707 | AIRCRAFT EQUIPMENT: De-Icers (Code 8/6): De-icing and anti-icing of aircraft propellers: investigation into fluid and ... | 1/1/1944 | 31/12/1949 | Res/Air/6747 |
AVIA 15/2916 | RESCUE (Code 44): Rotol variable pitch marine propellers: desirability of development for use in air ... | 1/1/1943 | 31/12/1943 | Res/Eng/4004 |
AVIA 15/2938 | ENGINES: Gas Turbine Engine (Code 22/2): Coupled turbine propeller units: development and reduction gear problems | 1/1/1946 | 31/12/1946 | Res/Eng/7991 |
AVIA 15/3258 | AIRCRAFT: Design and Development: General (Code 6/1): Centrifugally cast steel propeller barrels: design and trials | 1/1/1942 | 31/12/1945 | Res/Mat/598 |
AVIA 15/3258 | COMMITTEES AND COMMISSIONS: Home (Code 15/1): Centrifugally cast steel propeller barrels: design and trials | 1/1/1942 | 31/12/1945 | Res/Mat/598 |
AVIA 15/3434 | ENGINES: Production and Manufacture (Code 22/3): Rotol contra-rotating propellers: proposed nomenclature | 1/1/1942 | 31/12/1947 | Res/Pro/64 |
AVIA 15/3435 | ENGINES: Research and Development (Code 22/1): Centrifugally cast steel propeller barrels: development | 1/1/1941 | 31/12/1946 | Res/Pro/68 |
AVIA 15/3436 | ENGINES: Research and Development (Code 22/1): Standardisation of propeller spinners: discussions | 1/1/1941 | 31/12/1942 | Res/Pro/96 |
AVIA 15/3445 | ENGINES: Research and Development (Code 22/1): Single piece propeller barrel and spider for Mosquito: development | 1/1/1942 | 31/12/1942 | Res/Pro/143 |
AVIA 15/3446 | ENGINES: Research and Development (Code 22/1): Rotol variable pitch propellers: replacement of magnesium blades by ... | 1/1/1942 | 31/12/1947 | Res/Pro/145 |
AVIA 15/3447 | ENGINES: Research and Development (Code 22/1): Engine and propeller controls: development of inter-connection | 1/1/1943 | 31/12/1949 | Res/Pro/185 |
AVIA 15/3449 | ENGINES: Research and Development (Code 22/1): Gear driven contra-rotating propellers: report by DeHavilland Aircraft Co. ... | 1/1/1942 | 31/12/1944 | Res/Pro/207 |
AVIA 15/3451 | ENGINES: Research and Development (Code 22/1): Wood and metal propeller blades: investigation and reports on ... | 1/1/1942 | 31/12/1943 | Res/Pro/217 |
AVIA 15/3452 | ENGINES: Research and Development (Code 22/1): Propeller braking: design and tests | 1/1/1943 | 31/12/1947 | Res/Pro/219 Part I |
AVIA 15/3453 | ENGINES: Research and Development (Code 22/1): Propeller braking: design and tests | 1/1/1947 | 31/12/1953 | Res/Pro/219 Part II |
AVIA 15/3461 | ENGINES: Research and Development (Code 22/1): Reversible-pitch propellers: American development | 1/1/1943 | 31/12/1948 | Res/Pro/386 |
AVIA 15/3462 | ENGINES: Research and Development (Code 22/1): Reversible pitch braking propellers: ground and flight tests on ... | 1/1/1943 | 31/12/1949 | Res/Pro/395 |
AVIA 15/3463 | ENGINES: Research and Development (Code 22/1): Gearmatic propeller: introduction of new project by De Havillands | 1/1/1943 | 31/12/1945 | Res/Pro/400 |
AVIA 15/3464 | ENGINES: Research and Development (Code 22/1): Reversible pitch propellers: braking tests on Lancaster aircraft | 1/1/1943 | 31/12/1949 | Res/Pro/406 |
AVIA 15/3465 | ENGINES: Research and Development (Code 22/1): Propeller blades: report on American draw-rolling process | 1/1/1944 | 31/12/1944 | Res/Pro/411 |
AVIA 15/3466 | ENGINES: Production and Manufacture (Code 22/3): Engine propeller shafts: co-ordination of British and American standardisation | 1/1/1944 | 31/12/1949 | Res/Pro/450 |
AVIA 15/3467 | ENGINES: Research and Development (Code 22/1): Constant speed and hydromatic propellers for Barracuda: development of ... | 1/1/1939 | 31/12/1944 | Res/Pro/540 part I |
AVIA 15/3468 | ENGINES: Research and Development (Code 22/1): Constant speed and hydromatic propellers for Barracuda: development of ... | 1/1/1944 | 31/12/1949 | Res/Pro/540 part II |
AVIA 15/3469 | ENGINES: Research and Development (Code 22/1): Manually operated variable pitch propellers: development | 1/1/1945 | 31/12/1949 | Res/Pro/546 |
AVIA 15/3470 | AIRCRAFT EQUIPMENT: De-Icers (Code 8/6): Propeller electrical de-icing equipment: service trials | 1/1/1945 | 31/12/1951 | Res/Pro/611 |
AVIA 15/3471 | AIRCRAFT EQUIPMENT: De-Icers (Code 8/6): Electric de-icing of propellers: development | 1/1/1946 | 31/12/1948 | Res/Pro/697 |
AVIA 15/3878 | CIVIL AVIATION (Code 14): Propeller requirements in Civil aircraft | 1/1/1946 | 31/12/1948 | Sec/Pro/1 |
AVIA 15/3878 | ENGINES: Production and Manufacture (Code 22/3): Propeller requirements in Civil aircraft | 1/1/1946 | 31/12/1948 | Sec/Pro/1 |
AVIA 18/1320 | Determination of propeller power coefficients on Spitfire V C aircraft: flight tests | 1/1/1944 | 31/12/1944 | A&AEE/Res. 199 |
AVIA 18/2742 | Lincoln B Mk11 (Merlin 68): propeller surging tests with AY 202/A and AY 203/A constant ... | 1/1/1946 | 31/12/1946 | 822A 824 |
AVIA 18/2808 | Sea Fury Mk X SR 661 (Centaurus 12 SM): brief handling trials with modified propeller ... | 1/1/1945 | 31/12/1945 | 830 832 |
AVIA 18/3659 | Wyvern TF Mk 2 VP.109 (Python): assessment of improved engine-propeller response characteristics | 1/1/1949 | 31/12/1949 | 853/1 Pt 5 |
AVIA 19/1178 | Seaford flying boat: full scale spray tests with special reference to propeller damage | 1/1/1947 | 31/12/1947 | Report Reference F/Res/207 |
AVIA 19/283 | The changing of propellers and radiators on a moored Southampton seaplane | 1/1/1927 | 31/12/1927 | Report Reference F/A/38 |
AVIA 19/304 | Durability trial of experimental coating for propellers | 1/1/1927 | 31/12/1927 | Report Reference F/A/59 |
AVIA 19/880 | Value of reversible pitch propellers on seaplanes | 1/1/1944 | 31/12/1944 | Report Reference H/Res/178 |
AVIA 2/2779 | AIR MINISTRY: ADMINISTRATIVE: Consideration of turbine propeller short haul aircraft (Brabazon II B) prototype policy ... | 1/1/1945 | 31/12/1946 | Code no: 5/1 R.5474 |
AVIA 2/2779 | AIRCRAFT: Development and Trials: Consideration of turbine propeller short haul aircraft (Brabazon IIB) prototype; policy ... | 1/1/1945 | 31/12/1946 | Code No.6/1 R.5474 |
AVIA 28/2002 | Full-scale altitude test rig: replacement of present air turbine fan brake by a variable pitch ... | 1/1/1948 | 31/12/1948 | 8420/23 |
AVIA 28/2356 | Variable area propelling nozzles for use with reheat | 1/1/1944 | 31/12/1944 | M 1018 |
AVIA 28/2455 | Simple jet engine and two propeller turbine engines: comparison of performance as power plants for ... | 1/1/1945 | 31/12/1945 | M 1117 |
AVIA 28/2563 | Spill-off' variable propelling nozzle | 1/1/1946 | 31/12/1946 | R 7 |
AVIA 28/2588 | Combustion chamber for 250 HP propeller-turbine engine (CP 35) | 1/1/1946 | 31/12/1946 | S 5 |
AVIA 28/2590 | Fedden 1350 HP propeller turbine engine: design and development of combustion system | 1/1/1947 | 31/12/1947 | S 7 |
AVIA 28/3203 | Choice of propeller turbine engine for Naval reconnaissance aircraft | 1/1/1946 | 31/12/1946 | M9 |
AVIA 28/945 | Bristol Janus propeller turbine engine: netting report | 1/1/1946 | 31/12/1946 | 2 |
AVIA 38/535 | Patents: Curtis steel-bladed propellers | 1/1/1941 | 31/12/1941 | |
AVIA 38/623 | Analysis of airframe, engine and propeller purchases in USA 1939-1945 | 1/1/1945 | 31/12/1945 | |
AVIA 38/662 | Propellers | 1/1/1940 | 31/12/1941 | |
AVIA 38/753 | Propellers | 1/1/1940 | 31/12/1942 | |
AVIA 38/832 | Rotol propellers | 1/1/1941 | 31/12/1941 | |
AVIA 38/836 | Singer propellers | 1/1/1941 | 31/12/1941 | |
AVIA 38/852 | Propellers | 1/1/1941 | 31/12/1942 | |
AVIA 40/2546 | TRIEBWERK (engine propeller unit) | 1/1/1944 | 31/12/1944 | |
AVIA 44/465 | Engine and propeller vibrations | 1/1/1949 | 31/12/1949 | 2/4/2011 |
AVIA 44/495 | Propeller design: structural aspects | 1/1/1947 | 31/12/1947 | 2/7/2018 |
AVIA 44/581 | De Havilland Propellers, Ltd: propeller development, 1940-1945 | 1/1/1947 | 31/12/1947 | 16.01 |
AVIA 44/582 | De Havilland Propellers, Ltd: development and production of variable pitch propellers, 1939-1945 | 1/1/1949 | 31/12/1949 | 16.02 |
AVIA 46/211 | Propellers: development and production | 1/1/1934 | 31/12/1946 | 1/HIST/204 |
AVIA 46/83 | Development and production of propellers: narrative sources | 1/1/1942 | 31/12/1943 | 1/HIST/70 pt 1 |
AVIA 46/84 | Development and production of propellers: narrative sources | 1/1/1941 | 31/12/1942 | 1/HIST/70 pt 2 |
AVIA 54/114 | Propellers | 1/1/1947 | 31/12/1951 | 7/Aircraft/1431/10 Pt 1 |
AVIA 54/167 | Propellers | 1/1/1946 | 31/12/1957 | 7/Aircraft/ 2301/10 |
AVIA 54/235 | Propellers | 1/1/1946 | 31/12/1950 | 7/Aircraft/2781/10 Pt 1 |
AVIA 54/243 | Propellers | 1/1/1947 | 31/12/1956 | 7/Aircraft/2781/10 Annex to Pt 8 |
AVIA 54/25 | Propellers | 1/1/1946 | 31/12/1954 | 7/Aircraft/561/10 |
AVIA 54/54 | Propellers | 1/1/1946 | 31/12/1951 | 7/Aircraft/621/10 Pt 1 |
AVIA 54/63 | Propellers | 1/1/1946 | 31/12/1950 | 7/Aircraft/681/10 Pt 1 |
AVIA 54/76 | Propellers | 1/1/1946 | 31/12/1953 | 7/Aircraft/761/10 Pt 1 |
AVIA 6/10009 | Effect of contra rotation and nacelle interference on normal force of an inclined propeller: wind ... | 1/1/1947 | 31/12/1947 | 2191 |
AVIA 6/10035 | Effect of propeller thrust on downwash and velocity at tailplane | 1/1/1947 | 31/12/1947 | 2218 |
AVIA 6/10069 | Wind tunnel investigations of entry loss on propeller turbine installation, pt 1: annular entries behind ... | 1/1/1948 | 31/12/1948 | AERO REPORTS 2252 |
AVIA 6/10088 | Value of increased numbers of blades for propellers which operate at great altitudes | 1/1/1942 | 31/12/1942 | TN Aero 963 |
AVIA 6/10089 | Contra-rotating propellers: model tests | 1/1/1942 | 31/12/1942 | TN Aero 964 |
AVIA 6/10102 | Effect of compressibility on performance of propellers | 1/1/1942 | 31/12/1942 | TN Aero 977 |
AVIA 6/10104 | Effect of oxygen boosting on performance of propeller of Spitfire V and IV aircraft | 1/1/1942 | 31/12/1942 | TN Aero 979 |
AVIA 6/10115 | Effect of stalling of propeller on climb performance of fighters | 1/1/1942 | 31/12/1942 | TN Aero 990 |
AVIA 6/10122 | Propeller design problems of high speed aeroplanes | 1/1/1942 | 31/12/1942 | TN Aero 997 |
AVIA 6/10127 | Propeller efficiences: wind tunnel investigation of several factors affecting the performance of a high speed ... | 1/1/1942 | 31/12/1942 | TN Aero 1002 |
AVIA 6/10148 | Propeller aids to cooling of radial engines | 1/1/1942 | 31/12/1942 | TN Aero 1023 |
AVIA 6/10158 | Propeller locks and pitch indicators | 1/1/1942 | 31/12/1942 | TN Aero 1033 1033a |
AVIA 6/10184 | Propeller selection from aerodynamic considerations: comments | 1/1/1942 | 31/12/1942 | TN Aero 1059 |
AVIA 6/10210 | Aerodynamic problems in design of efficient propellers: comments | 1/1/1942 | 31/12/1942 | TN Aero 1086 |
AVIA 6/10211 | Effect of propeller operation on airflow in region of tailplane for a twin engine tractor ... | 1/1/1942 | 31/12/1942 | TN Aero 1087 |
AVIA 6/10224 | Propellers for Firefly aircraft | 1/1/1942 | 31/12/1942 | TN Aero 1100 |
AVIA 6/10229 | Wind tunnel tests of single and dual rotating tractor propellers of large blade width: comments | 1/1/1943 | 31/12/1943 | TN Aero 1105 |
AVIA 6/10243 | Propeller forces due to yaw and their effect on airplane stability | 1/1/1943 | 31/12/1943 | TN Aero 1119 |
AVIA 6/10263 | Use of reversible pitch propellers as air brakes | 1/1/1943 | 31/12/1943 | TN Aero 1139 |
AVIA 6/10276 | Effect of oxygen boosting at high altitude on performance of propellers for Spitfire IX aircraft | 1/1/1943 | 31/12/1943 | TN Aero 1153 |
AVIA 6/10278 | Effect of pitch on force and moment characteristics of full scale propellers of five solidities: ... | 1/1/1943 | 31/12/1943 | TN Aero 1155 |
AVIA 6/10288 | Analysis of flutter conditions on model high tip speed propellers | 1/1/1943 | 31/12/1943 | TN Aero 1165 |
AVIA 6/10289 | Propeller flutter | 1/1/1943 | 31/12/1943 | TN Aero 1166 |
AVIA 6/10328 | Propellers for Spitfire 21 with Griffon 61 engine with special reference to four and five ... | 1/1/1943 | 31/12/1943 | TN Aero 1206 |
AVIA 6/10333 | Charts for determination of efficiency of propeller over a range of speeds | 1/1/1943 | 31/12/1943 | TN Aero 1211 |
AVIA 6/10340 | Propeller designs for Welkin aircraft R.M.15 S.M. engines | 1/1/1943 | 31/12/1943 | TN Aero 1218 |
AVIA 6/10352 | Aerofoil data for propeller analysis | 1/1/1943 | 31/12/1943 | TN Aero 1230 |
AVIA 6/10401 | Charts for determination of static and take-off thrust of propeller | 1/1/1943 | 31/12/1943 | TN Aero 1281 1281a |
AVIA 6/10410 | Effect of compressibility on performance of propellers: further tables of 24 ft wind tunnel results | 1/1/1943 | 31/12/1943 | TN Aero 1290 |
AVIA 6/10411 | Comparison of propeller and ducted fan applied to a gas turbine | 1/1/1943 | 31/12/1943 | TN Aero 1291 |
AVIA 6/10464 | Comparison of experimental and calculated lift forces on an inclined propeller | 1/1/1943 | 31/12/1943 | TN Aero 1346 |
AVIA 6/10494 | Increase of tail area as means of recovering stability losses due to modern propellers at ... | 1/1/1944 | 31/12/1944 | TN Aero 1376 |
AVIA 6/10498 | Twin-engined aircraft fitted with reversed pitch propellers: wind tunnel tests | 1/1/1944 | 31/12/1944 | TN Aero 1380 |
AVIA 6/10514 | Influence of propeller fin effect on trend of single-engined fighter design | 1/1/1944 | 31/12/1944 | TN Aero 1396 |
AVIA 6/10537 | Mosquito propeller blades: summary of De Havilland report with some additional calculations | 1/1/1944 | 31/12/1944 | TN Aero 1419 |
AVIA 6/10538 | Effect of differing thickness distribution on a propeller's efficiency | 1/1/1944 | 31/12/1944 | TN Aero 1420 |
AVIA 6/10545 | Fluctuation of flow behind propeller at high advance | 1/1/1944 | 31/12/1944 | TN Aero 1427 |
AVIA 6/10547 | Single-engined fighter with reversed pitch propellers for landing: wind tunnel tests | 1/1/1944 | 31/12/1944 | TN Aero 1429 |
AVIA 6/10567 | Effect of compressibility on performance of propellers | 1/1/1944 | 31/12/1944 | TN Aero 1449 |
AVIA 6/10573 | High speed fighter propeller research programme: 2nd progress report | 1/1/1944 | 31/12/1944 | TN Aero 1455 |
AVIA 6/10605 | Cooling behind contra rotating propellers | 1/1/1944 | 31/12/1944 | TN Aero 1488 |
AVIA 6/10634 | Proposals for work on problems involved in propeller-turbine combinations | 1/1/1944 | 31/12/1944 | TN Aero 1517 |
AVIA 6/10639 | Comparision of methods for estimating static and take-off thrust of propeller | 1/1/1944 | 31/12/1944 | TN Aero 1522 |
AVIA 6/10656 | Application of linear perturbation theory to determine effect of compressibility on wind tunnel constraint on ... | 1/1/1944 | 31/12/1944 | TN Aero 1539 |
AVIA 6/10688 | Estimation of compressibility losses on propeller blade roots | 1/1/1944 | 31/12/1944 | TN Aero 1572 |
AVIA 6/10699 | Calibration of two-blade Rotol electric Typhoon propeller in 24ft tunnel | 1/1/1945 | 31/12/1945 | TN Aero 1583 |
AVIA 6/10701 | Methods of obtaining aerofoil section data for propellers with particular reference to stalled regime | 1/1/1945 | 31/12/1945 | TN Aero 1586 |
AVIA 6/10705 | Blockage effect on propellers of two motor nacelles in 24ft tunnel | 1/1/1945 | 31/12/1945 | TN Aero 1590 |
AVIA 6/10722 | Effect of compressibility on performance of propellers: tables of 24ft wind tunnel results with appendix ... | 1/1/1945 | 31/12/1945 | TN Aero 1607 |
AVIA 6/10736 | Review of the position of 200hp electric motor for driving propellers in high speed wind ... | 1/1/1945 | 31/12/1945 | TN Aero 1621 |
AVIA 6/10741 | Estimation of characteristics of NACA 16 propeller sections based on flight performance trials | 1/1/1945 | 31/12/1945 | TN Aero 1626 |
AVIA 6/10744 | Mean lift and drag data for stalled propellers | 1/1/1945 | 31/12/1945 | TN Aero 1629 |
AVIA 6/10747 | Range and speed of Windsor aircraft fitted with either four Merlin 100 reciprocating or four ... | 1/1/1945 | 31/12/1945 | TN Aero 1632 |
AVIA 6/10768 | Analysis of some low tip speed tests on propeller with NACA 16 series sections | 1/1/1945 | 31/12/1945 | TN Aero 1653 |
AVIA 6/10795 | Propeller efficiencies at high forward speeds | 1/1/1945 | 31/12/1945 | TN Aero 1680 |
AVIA 6/10812 | Full-scale propeller at negative pitch: wind tunnel tests | 1/1/1945 | 31/12/1945 | TN Aero 1697 |
AVIA 6/10822 | Assessment of value of pusher propellers to the aircraft designer | 1/1/1945 | 31/12/1945 | TN Aero 1707 |
AVIA 6/10834 | Pressure measurements on tow propeller blade roots | 1/1/1945 | 31/12/1945 | TN Aero 1719 |
AVIA 6/10843 | Rotol metal Spitfire propeller: results and data for single radius calculations from 24ft tunnel test | 1/1/1945 | 31/12/1945 | TN Aero 1728 |
AVIA 6/10852 | Wind tunnel measurements of internal loss on full-scale model of wing root intake duct for ... | 1/1/1945 | 31/12/1945 | TN Aero 1737 |
AVIA 6/10868 | Fixed pitch pusher propeller coupled to a free running turbine: design | 1/1/1946 | 31/12/1946 | TN Aero 1754 |
AVIA 6/10882 | Results of 24ft wind tunnel tests on 15% constant thickness propeller | 1/1/1946 | 31/12/1946 | TN Aero 1769 |
AVIA 6/10886 | Performance of stalled propellers: results and analysis of some 24ft. tunnel tests | 1/1/1946 | 31/12/1946 | TN Aero 1773 |
AVIA 6/10893 | Rotal wooden Spitfire propeller: 24ft tunnel test results and data for single radius calculations | 1/1/1946 | 31/12/1946 | TN Aero 1780 |
AVIA 6/10898 | Body interference on tractor propeller | 1/1/1946 | 31/12/1946 | TN Aero 1785 |
AVIA 6/10919 | Comparison of measured and calculated twist along a propeller blade | 1/1/1946 | 31/12/1946 | TN Aero 1806 |
AVIA 6/10922 | Comparison of alternative methods of coupling two gas turbines to drive a single contra-propeller | 1/1/1946 | 31/12/1946 | TN Aero 1809 |
AVIA 6/10930 | Determination of propeller efficiency in flight: tests with a Rotol propeller | 1/1/1946 | 31/12/1946 | TN Aero 1817 |
AVIA 6/10954 | Results of tests on a model propeller in the high speed tunnel: comments | 1/1/1946 | 31/12/1946 | TN Aero 1841 |
AVIA 6/10960 | Propellers with simulated ice and de-icing overshoes: comparative tests | 1/1/1946 | 31/12/1946 | TN Aero 1847 |
AVIA 6/10962 | Analysis of German tests on swept back propellers | 1/1/1946 | 31/12/1946 | TN Aero 1849 |
AVIA 6/10964 | Validity of full scale propeller braking tests | 1/1/1946 | 31/12/1946 | TN Aero 1851 |
AVIA 6/11011 | Comparative performances of propeller turbines, jet turbines and open fan augmentor power plants at 20,000 ... | 1/1/1947 | 31/12/1947 | TN Aero 1899 |
AVIA 6/11012 | Comparison of transonic drags obtained from dropped body tests and from analysis of propeller tests | 1/1/1947 | 31/12/1947 | TN Aero 1900 |
AVIA 6/11504 | Fluttering propellers: wind tunnel tests | 1/1/1943 | 31/12/1943 | SME 3231 |
AVIA 6/11523 | Fluttering propellers: spinning tests | 1/1/1943 | 31/12/1943 | SME 3254 |
AVIA 6/11535 | Failure of propeller blades in flutter | 1/1/1943 | 31/12/1943 | SME 3266 |
AVIA 6/11538 | Use of electrical strain gauges in propeller research and development | 1/1/1943 | 31/12/1943 | SME 3269 |
AVIA 6/11553 | Comparison of flutter characteristics of propeller when spun on electric motor and on engine | 1/1/1944 | 31/12/1944 | SME 3284 |
AVIA 6/11556 | Propellers with 2, 3 and 4 blades: comparison of flutter tests | 1/1/1944 | 31/12/1944 | SME 3287 |
AVIA 6/11585 | Detection of propeller flutter on spinning tower by use of strain gauges | 1/1/1945 | 31/12/1945 | SME 3318 |
AVIA 6/11604 | Centrifugal counter weights for propeller blades: design | 1/1/1945 | 31/12/1945 | SME 3337 |
AVIA 6/11626 | Concentration of strain at base of threads of metal propeller blade | 1/1/1946 | 31/12/1946 | SME 3360 |
AVIA 6/11662 | Strain gauge investigation of propeller flutter | 1/1/1947 | 31/12/1947 | SME 3399 |
AVIA 6/11665 | Coupled flexural vibrations of blades of propeller and torsional vibrations of engine crankshaft system | 1/1/1942 | 31/12/1942 | SME 4018 |
AVIA 6/11666 | Engine-propeller vibrations | 1/1/1942 | 31/12/1942 | SME 4019 |
AVIA 6/11667 | Frequency admittance curves for engine crankshaft, torsional and contra-revolving propeller-flexural vibration | 1/1/1943 | 31/12/1943 | SME 4020 |
AVIA 6/11671 | Effect of flexibility of propeller blades in coupled pitching and yawing vibrations of an aircraft | 1/1/1945 | 31/12/1945 | SME 4024 |
AVIA 6/11699 | Tomahawk - Allison V 1710-C15 aircraft: development of hydulignum wooden blades as replacement for steel ... | 1/1/1942 | 31/12/1942 | TN SME 79 |
AVIA 6/11700 | Tables for calculating interference velocity for condition of zero advance associated with a propeller with ... | 1/1/1942 | 31/12/1942 | TN SME 80 |
AVIA 6/11706 | Static thrust of a propeller | 1/1/1942 | 31/12/1942 | TN SME 91 |
AVIA 6/11724 | Elimination of flutter from propeller with laminated wood blades | 1/1/1943 | 31/12/1943 | TN SME 124 |
AVIA 6/11730 | Propeller pitch changing systems | 1/1/1943 | 31/12/1943 | TN SME 132 |
AVIA 6/11760 | Method of stressing laminated non-homogeneous propeller blade | 1/1/1943 | 31/12/1943 | TN SME 170 |
AVIA 6/11761 | 2nd fluttering propeller: spinning tests | 1/1/1943 | 31/12/1943 | TN SME 171 |
AVIA 6/11777 | 3rd fluttering propeller: spinning tests | 1/1/1943 | 31/12/1943 | TN SME 191 |
AVIA 6/11784 | 3 propellers of identical design: flutter tests | 1/1/1943 | 31/12/1943 | TN SME 198 |
AVIA 6/11788 | Climbing condition of aircraft as stressing case for propeller blades | 1/1/1943 | 31/12/1943 | TN SME 203 |
AVIA 6/11798 | Stressing of non-homogeneous propeller blades | 1/1/1944 | 31/12/1944 | TN SME 213 |
AVIA 6/11814 | Single stressing case for propeller when used as landing brake | 1/1/1944 | 31/12/1944 | TN SME 234 |
AVIA 6/11821 | New type of propeller blade root end: tests | 1/1/1944 | 31/12/1944 | TN SME 243 |
AVIA 6/11858 | Propeller flutter with strain gauges: investigation | 1/1/1944 | 31/12/1944 | TN SME 284 |
AVIA 6/11861 | Concentration of strain at base of threads of metal propeller blade | 1/1/1944 | 31/12/1944 | TN SME 288 |
AVIA 6/11876 | New type of propeller blade root end: further tests | 1/1/1945 | 31/12/1945 | TN SME 304 |
AVIA 6/11891 | Protection of propellers against ice | 1/1/1945 | 31/12/1945 | TN SME 320 |
AVIA 6/11909 | Flutter failures of propeller blades for A.R.C. fighter aircraft | 1/1/1945 | 31/12/1945 | TN SME 340 |
AVIA 6/11913 | Centrifugal counter-weights on V.D.M. propeller blades | 1/1/1945 | 31/12/1945 | TN SME 344 |
AVIA 6/11915 | Natural frequencies of Hamilton 3-paddle bladed propeller coupled with Merlin 85 engine | 1/1/1946 | 31/12/1946 | TN SME 346 |
AVIA 6/11916 | Wood propeller blade: bending test | 1/1/1946 | 31/12/1946 | TN SME 348 |
AVIA 6/11921 | Rotol propeller for Bristol 170 Hercules aircraft: strain gauge tests | 1/1/1946 | 31/12/1946 | TN SME 354 |
AVIA 6/11928 | Jablo wood propeller blades: bending and torsion tests | 1/1/1946 | 31/12/1946 | TN SME 361 |
AVIA 6/11932 | V.D.M. swept-back propeller blade design | 1/1/1946 | 31/12/1946 | TN SME 365 |
AVIA 6/1250 | Note on tandem propellers | 1/1/1917 | 31/12/1917 | B.A.171 |
AVIA 6/1254 | Preliminary report on the performance of BE 2c aircraft with variable pitch propeller | 1/1/1917 | 31/12/1917 | B.A.176 |
AVIA 6/1283 | Resumé of work at the Royal Aircraft Establishment on variable pitch propellers | 1/1/1918 | 31/12/1918 | B.A.237 |
AVIA 6/13076 | Flexural vibration characteristics of Rotol propeller coupled with torsional vibrations of Rolls-Royce 12 cylinder ... | 1/1/1945 | 31/12/1945 | Vib 6 |
AVIA 6/13082 | Engine and propeller vibrations | 1/1/1949 | 31/12/1949 | Vib 12 |
AVIA 6/13089 | Propeller vibrations: typical calculation of rotation coefficients | 1/1/1945 | 31/12/1945 | T.N.Vib 7 |
AVIA 6/13098 | Determination of fixed root frequencies of propeller blades using scale models and results compared with ... | 1/1/1945 | 31/12/1945 | T.N.Vib 16 |
AVIA 6/1347 | Spinning test on detachable bladed propeller by British and Colonial aeroplane company | 1/1/1920 | 31/12/1920 | B.A.353 |
AVIA 6/1351 | Spinning test on bullet-holed Dragonfly propeller | 1/1/1920 | 31/12/1920 | B.A.357 |
AVIA 6/1353 | Spinning tests on Cammell Laird variable pitch propeller | 1/1/1920 | 31/12/1920 | B.A.359 |
AVIA 6/1354 | Spinning test on Oddy detachable bladed propeller | 1/1/1920 | 31/12/1920 | B.A.360 |
AVIA 6/1355 | Spinning tests on Padouk propellers received from India | 1/1/1920 | 31/12/1920 | B.A.361 |
AVIA 6/1359 | Spinning tests on bullet-holed propellers | 1/1/1920 | 31/12/1920 | B.A.364 |
AVIA 6/1362 | Spinning tests on hollow steel propellers by Messrs. Armstrong Whitworth & Co | 1/1/1920 | 31/12/1920 | B.A.367 |
AVIA 6/14167 | Torsional vibration of crankshaft propeller systems in aircraft engines: investigation | 1/1/1923 | 31/12/1923 | E 3008 |
AVIA 6/14250 | Torsional vibration of crankshaft-propeller systems: brief review of technical position as affected by propeller-blade flexibility | 1/1/1942 | 31/12/1942 | T.N.ENG. 80 |
AVIA 6/14372 | German propeller types | 1/1/1946 | 31/12/1946 | SME 3358 |
AVIA 6/14382 | V.D.M. propeller from Heinkel 177 aircraft | 1/1/1944 | 31/12/1944 | TN SME 254 |
AVIA 6/14487 | Structural aspects of propeller design | 1/1/1947 | 31/12/1947 | REPORTS Structures 5 |
AVIA 6/14500 | 2, 3, 4 and 5 blade propellers: comparative flutter tests | 1/1/1948 | 31/12/1948 | REPORTS Structures 18 |
AVIA 6/14736 | Italian three blade variable pitch propeller: examination | 1/1/1943 | 31/12/1943 | TN SME 119 |
AVIA 6/14926 | Model spinning tests including tests with power unit driving propeller of six engined naval strike ... | 1/1/1948 | 31/12/1948 | R Aero 2271 |
AVIA 6/14931 | 24ft tunnel tests on propeller with NACA16 series sections. Test results and analysis into mean ... | 1/1/1948 | 31/12/1948 | R Aero 2276 |
AVIA 6/14936 | Wind tunnel investigation of entry loss on propeller turbine installations | 1/1/1948 | 31/12/1948 | R Aero 2281 |
AVIA 6/14975 | Slipstream effects at various tail positions on aircraft with four contra propellers | 1/1/1949 | 31/12/1949 | R Aero 2322 |
AVIA 6/14981 | Performance of a special de Havilland propeller on flight at high forward speeds | 1/1/1949 | 31/12/1949 | R Aero 2327 |
AVIA 6/14992 | Further high speed tunnel tests on a 1/15 scale model of E18/45 (DH 108), a ... | 1/1/1949 | 31/12/1949 | R Aero 2340 |
AVIA 6/1539 | Performance of Metal Propellers Ltd. steel blades to drg. MAC 10/26 type 94 Mk. 8 ... | 1/1/1925 | 31/12/1925 | B.A.544 |
AVIA 6/15600 | Cranking tests at low temperature of a propeller-gas turbine engine | 1/1/1949 | 31/12/1949 | TN ME 32 |
AVIA 6/15673 | Governing problems of turbine propellers | 1/1/1948 | 31/12/1948 | R ME 9 |
AVIA 6/16683 | Counter-rotating propellers in forced or crash landings | 1/1/1948 | 31/12/1948 | TN STRUCTURES: 19 |
AVIA 6/16702 | Electrical strain gauge circuits on metal propellers with particular reference to adhesives and damp resistants | 1/1/1949 | 31/12/1949 | TN STRUCTURES: 41 |
AVIA 6/16782 | Spinning tests of rotol hydraulic V.P. propeller for Viscount/Naiad | 1/1/1948 | 31/12/1948 | STRUCTURES TEST NOTES 228 |
AVIA 6/16888 | Propeller failures on Cirrus Major II engines | 1/1/1947 | 31/12/1947 | DEPT NOTE STRUCTURES ACCIDENT 213 |
AVIA 6/16920 | Vibration of turbine driven propeller systems: note for discussion by A.R.C. Oscillation Sub-Committee | 1/1/1949 | 31/12/1949 | TECH MEMOS STRUCTURES 40 |
AVIA 6/17092 | Spinning tests on rotol hydraulic co-axial VP propeller for Brabazon/Centaurus | 1/1/1946 | 31/12/1946 | TN SME 3432 |
AVIA 6/20083 | Kinetic temperature of propeller blades in conditions of icing | 1/1/1947 | 31/12/1947 | REPORTS ME 2 |
AVIA 6/21310 | Note on tandem propellers | 1/1/1917 | 31/12/1917 | REPORTS BA 171 |
AVIA 6/2463 | Test on drag of model propeller | 1/1/1918 | 31/12/1918 | WCN 6 |
AVIA 6/2488 | Experiments on a model variable pitch propeller | 1/1/1921 | 31/12/1921 | WCN 37 |
AVIA 6/2498 | Drag of stationary propellers | 1/1/1922 | 31/12/1922 | WCN 47 |
AVIA 6/2705 | The relative efficiencies of fast and slow moving propellers | 1/1/1916 | 31/12/1916 | H. 44, 44a |
AVIA 6/2733 | Note on T.722 'Relation between the efficiency of a propeller and its speed of retention' | 1/1/1916 | 31/12/1916 | H.201 |
AVIA 6/2887 | Action of castor oil on propeller varnishes | 1/1/1919 | 31/12/1919 | H.864 |
AVIA 6/3428 | Spinning tests on propeller finishing schemes | 1/1/1919 | 31/12/1919 | HC 524 |
AVIA 6/3442 | Rubbered fabric as a protective covering for propeller blades | 1/1/1920 | 31/12/1920 | HC 578 |
AVIA 6/3445 | Rubbered fabric for propeller blades | 1/1/1920 | 31/12/1920 | HC 582 |
AVIA 6/3456 | Japanese lacquer as protective covering for propeller blades | 1/1/1920 | 31/12/1920 | HC 601 |
AVIA 6/3466 | Japanese lacquer as protective covering for propeller blades | 1/1/1920 | 31/12/1920 | HC 613 |
AVIA 6/3475 | Burning wings in the slip stream from a propeller | 1/1/1921 | 31/12/1921 | HC 626 |
AVIA 6/3665 | Propeller finishing schemes | 1/1/1925 | 31/12/1925 | HC 891 |
AVIA 6/3669 | Propeller finishing schemes: exposure tests | 1/1/1925 | 31/12/1925 | HC 897 |
AVIA 6/4157 | Progress on propeller boss experiments on Hispano Suiza engines by Experimental Squadron, Royal Aircraft Establishment | 1/1/1918 | 31/12/1918 | K.1319 |
AVIA 6/4158 | Further report on propeller boss experiments on Hispano Suiza engines | 1/1/1918 | 31/12/1918 | K.1319A |
AVIA 6/4235 | Visual signalling for propeller starting on twin or multi-engined aeroplanes | 1/1/1921 | 31/12/1921 | K.1688 |
AVIA 6/4241 | Failure of propeller on Badger aircraft J/6492, 'Jupiter' engine No. 801/A/26466 | 1/1/1921 | 31/12/1921 | K.1702 |
AVIA 6/5512 | Vibration of propellers due to non-uniform inflow | 1/1/1942 | 31/12/1942 | E.3938 |
AVIA 6/5526 | Investigation into the possibility of reducing propeller blade vibration on Merlin power units by fitting ... | 1/1/1942 | 31/12/1942 | E.3955 |
AVIA 6/5541 | Admittance of a propeller of fan at a given frequency: a solution which takes account ... | 1/1/1943 | 31/12/1943 | E.3974 |
AVIA 6/5543 | Torsiograph observation on a Merlin 11 engine, using a serrated condenser pick-up, with five different ... | 1/1/1943 | 31/12/1943 | E.3976 |
AVIA 6/5558 | Comparative performance of a propeller turbine engine equipped with a series of heat exchangers | 1/1/1943 | 31/12/1943 | E.3993 |
AVIA 6/5563 | Comparative performance of propeller turbine engines of different design pressure ratio installed in a bomber ... | 1/1/1944 | 31/12/1944 | E.4000 |
AVIA 6/5574 | The merits of reheat and heat exchange in propeller turbine engines | 1/1/1944 | 31/12/1944 | E.4112 |
AVIA 6/5608 | Tests with De Havilland cuffed propeller on Wellington IC aeroplane | 1/1/1942 | 31/12/1942 | T.N.ENG.18 |
AVIA 6/5658 | Experimental determination of the modes of vibration of a model propeller | 1/1/1943 | 31/12/1943 | T.N.ENG.91 |
AVIA 6/5732 | Comparative performance of jet propulsion ducted fan and propeller turbine engines A.S.X. design | 1/1/1943 | 31/12/1943 | T.N.ENG.200 |
AVIA 6/5781 | Reduction gears for turbine driven propellers and fans | 1/1/1944 | 31/12/1944 | T.N.ENG.266 |
AVIA 6/5801 | Performance characteristics of propeller turbine engines with reheat and heat-exchange | 1/1/1944 | 31/12/1944 | T.N.ENG.292 |
AVIA 6/5851 | Investigation of engine cutting and propeller overspeeding of Barracuda 11 aircraft on entering and during ... | 1/1/1945 | 31/12/1945 | T.N.ENG. 357 |
AVIA 6/5979 | Experimental DH9a aircraft propellers for Middle East | 1/1/1923 | 31/12/1923 | MT3293 3293a |
AVIA 6/5980 | DH9a Liberty aircraft propeller fractured in the air at Shotwick | 1/1/1923 | 31/12/1923 | MT4112 |
AVIA 6/8092 | Note on examination of broken Fairey-Reed propeller FR.16221 | 1/1/1942 | 31/12/1942 | M 7429 |
AVIA 6/8093 | Cracked Fairey Reed propeller FR.16611 | 1/1/1942 | 31/12/1942 | M 7443 |
AVIA 6/8117 | Examination of corroded duralumin propeller blades from Lysander aircraft | 1/1/1942 | 31/12/1942 | M 7150 |
AVIA 6/8121 | Examination of root of broken magnesium alloy blade of Halifax propeller No.7689 | 1/1/1942 | 31/12/1942 | M 7109 |
AVIA 6/8123 | Examination of broken propeller No.7571 from Halifax aircraft | 1/1/1942 | 31/12/1942 | M 6973 |
AVIA 6/8130 | Examination of propeller blades in X76S alloy with special reference to the effect of cold ... | 1/1/1942 | 31/12/1945 | M 6922a |
AVIA 6/8131 | Stress corrosion tests on bent and straightened X76S and D.T.D.150 propeller blade materials | 1/1/1942 | 31/12/1945 | M 6922b |
AVIA 6/8172 | Examination of broken Fairey-Reed propeller FR.29314 | 1/1/1943 | 31/12/1943 | M 8365 |
AVIA 6/8215 | The effects of overheating on the mechanical properties of duralumin propeller blade material | 1/1/1943 | 31/12/1943 | M 7263a |
AVIA 6/8229 | Examination of two magnesium alloy propeller blades with particular reference to fatigue properties | 1/1/1943 | 31/12/1943 | M 6422 |
AVIA 6/8239 | Examination of sample of burnt alloy steel from propeller shaft | 1/1/1943 | 31/12/1943 | M 8083 |
AVIA 6/8248 | Examination of broken Fairey-Reed propeller FR.19274 | 1/1/1943 | 31/12/1943 | M 8204 |
AVIA 6/8270 | Failure of Hamilton propeller blade No. NK.22328 | 1/1/1944 | 31/12/1944 | M 8286 |
AVIA 6/8332 | Fatigue strength of duralumin propeller blade forgings to specification D.T.D.150 | 1/1/1945 | 31/12/1945 | M 6114 |
AVIA 6/8382 | Metallurgical examination of a centrifugally cast steel propeller barrel | 1/1/1945 | 31/12/1945 | M 9312 |
AVIA 6/8846 | Propeller | 1/1/1942 | 31/12/1942 | 14/34 |
AVIA 6/9009 | Hydraulic propeller pitch control gear | 1/1/1942 | 31/12/1942 | 41/23 |
AVIA 6/9043 | V.D.M. propeller | 1/1/1943 | 31/12/1943 | 44/11 |
AVIA 6/9057 | VDM 3 blade propeller | 1/1/1944 | 31/12/1944 | 44/25 |
AVIA 6/9107 | V.D.M. propeller | 1/1/1944 | 31/12/1944 | 200/1 |
AVIA 6/9254 | Description | 1/1/1946 | 31/12/1946 | 269/1 |
AVIA 6/9358 | Junkers Ju 88 propeller | 1/1/1942 | 31/12/1942 | 60 |
AVIA 6/9366 | Italian 3 blade variable pitch propeller | 1/1/1943 | 31/12/1943 | 72 |
AVIA 6/9593 | Contra-rotating propeller: tests in 24ft tunnel | 1/1/1942 | 31/12/1942 | 1751 |
AVIA 6/9637 | Compressibility drag data for propeller calculations | 1/1/1943 | 31/12/1943 | 1795 |
AVIA 6/9658 | Application of calculus of variations to propeller design | 1/1/1943 | 31/12/1943 | 1816 |
AVIA 6/9693 | New theory of propeller fin effect | 1/1/1943 | 31/12/1943 | 1851 |
AVIA 6/9702 | Supermarine F.1/43 aircraft: wind tunnel tests with propeller | 1/1/1943 | 31/12/1943 | 1860 |
AVIA 6/9706 | Tunnel measurements of propeller fin effects including effect on complete models | 1/1/1943 | 31/12/1943 | 1864 |
AVIA 6/9707 | Contribution of propellers to longitudinal and lateral derivatives of the aeroplane in absence of interference ... | 1/1/1943 | 31/12/1943 | 1865 |
AVIA 6/9721 | Supermarine F.1/43 aircraft: wind tunnel tests with five bladed propeller | 1/1/1943 | 31/12/1943 | 1889 |
AVIA 6/9724 | Use of combination of propeller and jet engines in long range fighters | 1/1/1943 | 31/12/1943 | 1892 |
AVIA 6/9727 | Aerofoil data for use in single radius propeller performance calculations | 1/1/1943 | 31/12/1943 | 1895 |
AVIA 6/9763 | De Havilland F.12/43 with various modes of propeller rotation, pt 1: without landing flaps | 1/1/1944 | 31/12/1944 | 1931 |
AVIA 6/9764 | Hawker F.2/43 aircraft: wind tunnel tests with propeller | 1/1/1944 | 31/12/1944 | 1932 |
AVIA 6/9766 | Charts to determine efficiency of propeller over a range of speeds | 1/1/1944 | 31/12/1944 | 1934 |
AVIA 6/9773 | Wind tunnel measurements of efficiency on contra-rotating propeller on a wing, pt 1: pusher propellers | 1/1/1944 | 31/12/1944 | 1941 |
AVIA 6/9776 | Suggested general method of treatment of static longitudinal stability with propellers: analysis of full throttle ... | 1/1/1944 | 31/12/1944 | 1944 |
AVIA 6/9777 | Sectional lift and drag data on 15% and 25% thick propeller sections | 1/1/1944 | 31/12/1944 | 1945 |
AVIA 6/9790 | Effect of propeller at zero torque on pitching and yawing moments of single engine fighter: ... | 1/1/1944 | 31/12/1944 | 1958 |
AVIA 6/9794 | Variation of lift coefficient of thin Clark Y propeller sections with Mach number and incidence | 1/1/1944 | 31/12/1944 | 1962 |
AVIA 6/9802 | 24ft tunnel tests of feathered contra-propeller | 1/1/1944 | 31/12/1944 | 1970 |
AVIA 6/9805 | Revised values of CL and CD for Clark Y sections for use in propeller strip ... | 1/1/1944 | 31/12/1944 | 1973 |
AVIA 6/9811 | Stability of a propeller governing system | 1/1/1944 | 31/12/1944 | 1979 |
AVIA 6/9816 | Data on propellers of N.A.C.A.16 series section at high rates of advance | 1/1/1944 | 31/12/1944 | 1984 |
AVIA 6/9822 | Performance of civil transport aircraft with reciprocating engines and with propeller turbine engines: comparison | 1/1/1944 | 31/12/1944 | 1990 |
AVIA 6/9833 | Tests in 8ft high speed tunnel of propeller N.A.C.A. 4-308-045: comments and analysis | 1/1/1944 | 31/12/1944 | 2001 |
AVIA 6/9844 | Wind tunnel measurements of efficiency of contra-rotating propeller on a wing, pt 2: tractor propeller | 1/1/1945 | 31/12/1945 | 2013 |
AVIA 6/9846 | Twin-engined aircraft with contra-rotating propellers: wind tunnel tests | 1/1/1945 | 31/12/1945 | 2015 |
AVIA 6/9850 | Wake and downwash behind wings and wing-body combinations without flaps or propellers: investigation | 1/1/1945 | 31/12/1945 | 2019 |
AVIA 6/9853 | Charts for determination of propeller efficiencies in climbing and cruising ranges | 1/1/1945 | 31/12/1945 | 2022 |
AVIA 6/9855 | Wind tunnel measurements of the forces on inclined propellers | 1/1/1945 | 31/12/1945 | 2024 |
AVIA 6/9865 | Wind tunnel tests on S.11/43 twin-engined aircraft with contra-rotating propellers, pt 1: general stability | 1/1/1945 | 31/12/1945 | 2034 2034a |
AVIA 6/9878 | Cowl entry losses on Hercules Beaufighter aircraft nacelle fitted with flared and unflared propellers: 24 ... | 1/1/1945 | 31/12/1945 | 2047 |
AVIA 6/9882 | Wind tunnel tests on S11/43 twin-engined aircraft with contra-rotating propellers, pt 2: tests on split, ... | 1/1/1945 | 31/12/1945 | 2051 |
AVIA 6/9905 | Lift characteristics for thin Clark Y propeller sections at low and negative angles of incidence | 1/1/1945 | 31/12/1945 | 2075 |
AVIA 6/9909 | Design of propeller turbine combinations, pt 1: Naval fighter | 1/1/1945 | 31/12/1945 | 2079 |
AVIA 6/9923 | Thrust and torque measurements on a 2 blade 6% thick Clarke Y section propeller: high ... | 1/1/1945 | 31/12/1945 | 2096 2096a |
AVIA 6/9926 | Design of propeller turbine combinations, pt 2: civil aircraft | 1/1/1945 | 31/12/1945 | 2099 |
AVIA 6/9942 | Longitudinal stability of single-engined aircraft with contra-rotating propeller: low speed wind tunnel tests | 1/1/1946 | 31/12/1946 | 2116 |
AVIA 6/9959 | Determination of static and take-off thrusts of a propeller: revised charts | 1/1/1946 | 31/12/1946 | 2135 |
AVIA 6/9988 | Single-engined Westland aircraft with contra rotating propellers: high speed wind tunnel tests | 1/1/1946 | 31/12/1946 | 2166 |
AVIA 6/9994 | Paddle blade propeller: 24ft tunnel tests | 1/1/1946 | 31/12/1946 | 2172 |
AVIA 6/9999 | Revised high speed lift and drag Clark Y section data for propeller performance calculations | 1/1/1947 | 31/12/1947 | 2177 |
AVIA 65/199 | DTD683 light alloy for propeller blades: investigation | 1/1/1947 | 31/12/1954 | AX/245/09PtA |
AVIA 65/201 | Propellers: research policy and 24ft wind tunnel work at RAE | 1/1/1947 | 31/12/1966 | AX/246/02PtA |
AVIA 7/2977 | Screening of test plant of aircraft engines and propellers at Farnborough | 1/1/1925 | 31/12/1927 | 303 |
AVIA 7/3226 | Location of ships by propeller and cruising sound | 1/1/1928 | 31/12/1935 | 1208 |
AVIA 72/1 | US-Canada-UK Conference, September | 1/1/1949 | 31/12/1949 | DMXRD REPORTS 2/49 |
AVIA 8/268 | Synchronising of machine gun and propeller blades by F W Scarff: patent application 7905/16 | 1/1/1916 | 31/12/1933 | S.32211 |
AVIA 8/410 | Hydraulic transmission by T Paterson between engine and propeller | 1/1/1935 | 31/12/1935 | 425940/35 |
AVIA 8/416 | Propelling aircraft by Dr A A Griffith and F W Meredith | 1/1/1936 | 31/12/1936 | S.38326 |
AVIA 8/84 | Propellers for aircraft and the like by Commodore M F Sueter, Lt. A Landells and ... | 1/1/1916 | 31/12/1933 | S.32268 |
AVIA 8/85 | Hart variable pitch propeller: investigation | 1/1/1917 | 31/12/1919 | A.I.C.I/1170 |
AVIA 8/86 | Propeller swinger: invention submitted by Aircraft Manufacturing Co. | 1/1/1918 | 31/12/1918 | A.I.C.5986 |
AVIA 8/87 | Variable pitch propeller and cable lock for controls: consideration of inventions submitted by E A ... | 1/1/1918 | 31/12/1919 | A.I.C.5462 |
AVIA 8/89 | Variable pitch propellers: progress of research work | 1/1/1924 | 31/12/1926 | 481678/24 |
AVIA 8/90 | Variable pitch propellers: progress of research work | 1/1/1926 | 31/12/1928 | 702463/26 |
AVIA 8/91 | Experiments on bi-convex metal airscrews for Condor, Jupiter and Jaguar engines by Messrs. Metal Propellers | 1/1/1927 | 31/12/1929 | 763331/27 |
AVIA 8/92 | Experiments on bi-convex metal airscrews for Condor, Jupiter and Jaguar engines by Messrs. Metal Propellers | 1/1/1929 | 31/12/1931 | 920904/29 |