The Aeronautical Journal, Volume 73Royal Aeronautical Society, 1969 - Aeronautics |
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Page 777
... landing with rearwards and sideways drift , to an emergency conventional landing onto a runway at speeds of the order of 150 knots ( 280 km / hr ) . Because of the necessity to carry maximum payloads into dispersed sites , the Design ...
... landing with rearwards and sideways drift , to an emergency conventional landing onto a runway at speeds of the order of 150 knots ( 280 km / hr ) . Because of the necessity to carry maximum payloads into dispersed sites , the Design ...
Page 935
... landing field length . The use of thrust reverse after touchdown was assumed , in accordance with British Airworthiness rules , in determining the landing performance . However , the rear engined layout offered the possibility of making ...
... landing field length . The use of thrust reverse after touchdown was assumed , in accordance with British Airworthiness rules , in determining the landing performance . However , the rear engined layout offered the possibility of making ...
Page 947
... landing field length . The use of thrust reverse after touchdown was assumed , in accordance with British Airworthiness rules , in determining the landing performance . However , the rear engined layout offered the possibility of making ...
... landing field length . The use of thrust reverse after touchdown was assumed , in accordance with British Airworthiness rules , in determining the landing performance . However , the rear engined layout offered the possibility of making ...
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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