The Aeronautical Journal, Volume 73Royal Aeronautical Society, 1969 - Aeronautics |
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Page 639
... reduced range . Loading and unloading is facilitated by the large cargo door . The certification is based on CAR , Part 3 , Normal Category . 7 . INVESTIGATIONS INTO THE REDUCTION OF TAKE - OFF AND LANDING DISTANCES BY SLIPSTREAM DEFLEC ...
... reduced range . Loading and unloading is facilitated by the large cargo door . The certification is based on CAR , Part 3 , Normal Category . 7 . INVESTIGATIONS INTO THE REDUCTION OF TAKE - OFF AND LANDING DISTANCES BY SLIPSTREAM DEFLEC ...
Page 651
... reducing equipment we get a distance of 2150 m ( 7100 ft ) which , however , could be reduced to 1500 m ( 4950 ft ) using mixing nozzles only . Installing mixing nozzles on the lift and propulsion engines , together with ejector lift ...
... reducing equipment we get a distance of 2150 m ( 7100 ft ) which , however , could be reduced to 1500 m ( 4950 ft ) using mixing nozzles only . Installing mixing nozzles on the lift and propulsion engines , together with ejector lift ...
Page 817
... reduced and reverse flow over the blade sections as indicated . When the flow is reversed , a download is created , adding to the problem or rotor balance . Reduced airflow demands operation at high lift coefficients where stall is ...
... reduced and reverse flow over the blade sections as indicated . When the flow is reversed , a download is created , adding to the problem or rotor balance . Reduced airflow demands operation at high lift coefficients where stall is ...
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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