Showing 66 items matching " farnborough"
-
Moorabbin Air MuseumManual (Item) - Focke Wulf FW190 fighter, Farnborough Report No. E.A.44/1 Superficial Examination of FW190.A3
Royal Aircraft Establishment, Farnborough -
Moorabbin Air Museum
Work on paper (Item) - Focke Wulf FW190 fighter, Royal Aircraft Establishment , Farnborough Notes on Discussion with the Staff of Focke-Wulf Ltd
Royal Aircraft Establishment, Farnborough -
Moorabbin Air MuseumDocument (item) - Farnborough Report No. Aero 1765: Model tests of flame damping screens for the Spitfire, and analysis of the results, July, 1942, Also addendum to above, Farnborough Report No. Aero 1765
Created during the middle of the Second World War (1942) about tests undertaken on flame damping screens for the exhausts of the Supermarine Spitfire. spitfire, farnborough, royal aircraft establishment -
Moorabbin Air MuseumDocument (item) - Farnborough Report No. Aero 1771: Flight tests of spring tab ailerons on a Spitfire, August, 1942, Farnborough Report No. Aero 1771: Flight tests of spring tab ailerons on a Spitfire
Create in August 1942, during the middle of the Second World War. A report created by the Royal Aircraft Establishment about the utilization of spring tab ailerons on the Supermarine Spitfire. supermarine spitfire, farnborough, second world war, royal aircraft establishment -
Bendigo Historical Society Inc.Postcard - BASIL WATSON COLLECTION: POSTCARD, B.E. TYPE 220 70 HP RENAULT
postcard: biplane, with crowd of people behind, sheds in background. Plane has 220 on rear. Written on top ' B.E. Type 220 70 H.P. Renault'John Drew, Aldersho & Farnborough, our aerial defence series 514aviation, civilian, 220 hp renault, basil watson collection, renault, farnborough -
Moorabbin Air Museum
Document (Item) - Farnborough Report No. Mat/N/1/3110 Tests On Aeroplastic Typhoon Seats August 1942
Description: Date: October 1942 Author: W. Tye Publisher: Royal Aircraft Establishment Pages: 4 Binding: Permanent/ Soft Keywords: RAE Report No. S. M. E. 3234 Level of Importance: National. File No.80 A -
Moorabbin Air Museum
Manual (item) - Sabre F86A CAC, Farnborough RAE, & NAA - Flight Controls, Air conditioning, Flight Manual & Tests
-
Moorabbin Air Museum
Booklet (Item) - Model Tests On The Vickers F7/41 High Altitude Fighter , Farnborough Report No. Aero 1741 , File No.4A
-
Moorabbin Air Museum
Manual (Item) - Loading Problems - symposium at Farnborough 1966 RAE
-
Moorabbin Air Museum
Booklet (Item) - Air Show - Farnborough 1968
-
Moorabbin Air Museum
Booklet (Item) - Air Show - Farnborough 1950 - 11th airshow
-
Moorabbin Air Museum
Manual (Item) - RAE Farnborough Notes on the Dog Fight S.B. Gates Report B.A.1613
-
Moorabbin Air Museum
Document (Item) - RAE Farnborough Analysis of Aileron Performance by S.B.Gates and H.B.Irving Report No B.A.1624
-
Moorabbin Air Museum
Essay (Item) - RAE Farnborough No BA 1621 Effects on the nose shape on the characteristics of Frise Ailerons H Davies and EC Brown
-
Moorabbin Air Museum
Document - Enemy Aircraft:- Dornier 217 E/1 Twin Engine Bomber No.U5DN, Examination of BMW 801A/1 Engine File No.17A, Farnborough Report No.EA. 41/22
-
Moorabbin Air Museum
Document (Item) - Tables for use in the investigation of supersonic fields of flow by the method of characteristics, Royal aircraft establishment Farnborough Hants
-
Moorabbin Air Museum
Document (Item) - Note on the problem of interception at high subsonic speeds, Royal aircraft establishment Farnborough Hants
-
Moorabbin Air Museum
Document (Item) - Aero 1092 SME 96 secret structure weight data and drag analysis for British and foreign aircraft, Royal aircraft establishment Farnborough Hants
-
Moorabbin Air Museum
Document (Item) - Aero 1348 Note on the various methods of performance reduction for jet propelled aircraft, Royal aircraft establishment Farnborough Hants
-
Moorabbin Air Museum
Document (Item) - Aero 1729 comparative effects of small changes in profile drag and weight on aircraft performance, Royal aircraft establishment Farnborough Hants
-
Moorabbin Air Museum
Document (Item) - Aero 1678 Wind tunnel 11.5ft wide x 8.5ft high testing calculations graphs design, Royal aircraft establishment Farnborough Hants
-
Moorabbin Air Museum
Document (Item) - SME 3279 the calculation of aileron reversal speed equations graphs, Royal aircraft establishment Farnborough Hants
-
Moorabbin Air Museum
Document (Item) - SME 3262 reversal of aileron control calculation methods, Royal aircraft establishment Farnborough Hants
-
Moorabbin Air Museum
Document (Item) - Farnborough Report No SME 3236 The Design of Smooth Wings, Royal aircraft establishment Farnborough Hants
-
Moorabbin Air Museum
Document (Item) - R A E Report No SME 3273 theoretical forces and moments on a thin aerofoil with hinged flap at supersonic speeds, Royal aircraft establishment Farnborough Hants
-
Moorabbin Air Museum
Document (Item) - R A E Report No SME 3199 a method of estimating the diect stress concentration round holes in reinforced sheet, Royal aircraft establishment Farnborough Hants
-
Moorabbin Air Museum
Document (Item) - R A E Report No SME 3255 the theoretical variation of pitching moment coefficient with mach number at zero lift, Royal aircraft establishment Farnborough Hants
-
Moorabbin Air Museum
Document (Item) - R A E Report No SME 3275 data for the design of smooth wing surfaces, Royal aircraft establishment Farnborough Hants
-
Moorabbin Air Museum
Document (Item) - R A E Report No SME 3271 the use of scale models for strength tests, Royal aircraft establishment Farnborough Hants
-
Moorabbin Air Museum
Document (Item) - Aero 1673 notes on a visit to southern Germany to interrogate German technical staff on stability and control matters with respect to flight testing, Royal aircraft establishment Farnborough Hants
