The Aeronautical Journal, Volume 73Royal Aeronautical Society, 1969 - Aeronautics |
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Page 623
... unit . The symbols are formed on the high intensity CRT . The optical system , a simple form of which is shown in Fig . 3 , forms an image of the CRT display at infinity in the pilot's line of sight . The EHT unit provides the high ...
... unit . The symbols are formed on the high intensity CRT . The optical system , a simple form of which is shown in Fig . 3 , forms an image of the CRT display at infinity in the pilot's line of sight . The EHT unit provides the high ...
Page 658
... unit layout , the excess thrust re- quired for control will reduce if the lift unit is mounted further from the aircraft axis . For example , roll control of the Dornier Do 31 aircraft ( Fig . 3 ) is achieved by differ- ential ...
... unit layout , the excess thrust re- quired for control will reduce if the lift unit is mounted further from the aircraft axis . For example , roll control of the Dornier Do 31 aircraft ( Fig . 3 ) is achieved by differ- ential ...
Page 784
... unit has been effectively duplicated at its most vulnerable point - the flexhose from engine to airframe . This hose is encased in a ball - jointed pressure - carrying tube which has a small vent to the aircraft skin . This vent is ...
... unit has been effectively duplicated at its most vulnerable point - the flexhose from engine to airframe . This hose is encased in a ball - jointed pressure - carrying tube which has a small vent to the aircraft skin . This vent 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