The Aeronautical Journal, Volume 73Royal Aeronautical Society, 1969 - Aeronautics |
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Page 678
... solution exact numerical solution www 2 3 46 48 ORBITS 4:04 0.4 0 : 00 : 0.4 Ki = 0,25 49 20 -20 20 -20 50 O www www www.w approximate analytical solution exact numerical solution • 2 3 4 ORBITS 46 4. 15 ° 0.10 : 10 ° 0 : 0.15 Ki : 0.25 ...
... solution exact numerical solution www 2 3 46 48 ORBITS 4:04 0.4 0 : 00 : 0.4 Ki = 0,25 49 20 -20 20 -20 50 O www www www.w approximate analytical solution exact numerical solution • 2 3 4 ORBITS 46 4. 15 ° 0.10 : 10 ° 0 : 0.15 Ki : 0.25 ...
Page 1002
... solution of the recirculation region and its coupling to the rest of the flow field results in the first known complete solution of the near wake , up to the rear stagnation point . The near wake is divided into three sub - regions ...
... solution of the recirculation region and its coupling to the rest of the flow field results in the first known complete solution of the near wake , up to the rear stagnation point . The near wake is divided into three sub - regions ...
Page 1003
... solution of the recirculation region and its coupling to the rest of the flow field results in the first known complete solution of the near wake , up to the rear stagnation point . The near wake is divided into three sub - regions ...
... solution of the recirculation region and its coupling to the rest of the flow field results in the first known complete solution of the near wake , up to the rear stagnation point . The near wake is divided into three sub - regions ...
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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