The Aeronautical Journal, Volume 73Royal Aeronautical Society, 1969 - Aeronautics |
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Page 639
... Figure 8. Do 28 A with skis . Figure 9. Do 28 with floats . Figure 10. Do 28 B. Figure 11. Do 28 D model in the wind tunnel . 18- CL = q.Sw 28 ° Figure 12 . Do. SILVIUS DORNIER 639 POST - WAR RESEARCH AND DEVELOPMENT AT DORNIER.
... Figure 8. Do 28 A with skis . Figure 9. Do 28 with floats . Figure 10. Do 28 B. Figure 11. Do 28 D model in the wind tunnel . 18- CL = q.Sw 28 ° Figure 12 . Do. SILVIUS DORNIER 639 POST - WAR RESEARCH AND DEVELOPMENT AT DORNIER.
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H2278 Figure 15. Avro 504 . 80 hp Clerget Engine . It was easily recognisable with its central undercarriage skid ... Figure 17. Bristol Fighter . N5438 Figure 18. Sopwith Triplane . CAPRONI 600 HP TRIPLANNO 1916 Figure 19. Caproni 600 ...
H2278 Figure 15. Avro 504 . 80 hp Clerget Engine . It was easily recognisable with its central undercarriage skid ... Figure 17. Bristol Fighter . N5438 Figure 18. Sopwith Triplane . CAPRONI 600 HP TRIPLANNO 1916 Figure 19. Caproni 600 ...
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Figure 27. HMS Slinger . Figure 25. Handley Page V1500 . Then came a spell of War Office Staff work . One of my ... Figure 28. Short 184 . Figure 29. Fairey F22 Campania . O N37 Figure 26. DH9 . Figure 30 . Norman Thompson N.1B . Իր ...
Figure 27. HMS Slinger . Figure 25. Handley Page V1500 . Then came a spell of War Office Staff work . One of my ... Figure 28. Short 184 . Figure 29. Fairey F22 Campania . O N37 Figure 26. DH9 . Figure 30 . Norman Thompson N.1B . Իր ...
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Aero aerodynamic aerofoil Aeronautical Journal aeroplane air transport airline airport angle application associated Aviation blade boundary layer British BRITISH AIRCRAFT CORPORATION cargo CEng civil Civil Air Transport configuration conventional cost cross-coupling dynamic effect engine equipment fibres field Figure flight flow flying FRAeS fuselage future Harrier Hawker Siddeley Aviation helicopter hover Illustrated increase industry lecture lift lift-fan London Mach number man-powered flight mechanical ment methods military NASA TN noise level obtained operation organisation outer space paper passengers performance pilot plate polymers possible present problem programme propulsion ratio rotorcraft Royal Aeronautical Society Royal Air Force satellite shown in Fig speed STOL structure Sud Aviation supersonic tail rotor take-off technical techniques Technology temperature thrust tion traffic turbine V/STOL vector vehicle velocity VTOL weight Westland wing