The Aeronautical Journal, Volume 73Royal Aeronautical Society, 1969 - Aeronautics |
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Page 619
... Flight Length ( 1966 ) yds 257 984 720 960 AUW lb 240 370 270 265 Wing Span ft 44.3 55.7 80 84 Prop diameter ft 4.9 ... flight is much the same as the position of powered flight in 1900. A few people know that it is possible , and as I ...
... Flight Length ( 1966 ) yds 257 984 720 960 AUW lb 240 370 270 265 Wing Span ft 44.3 55.7 80 84 Prop diameter ft 4.9 ... flight is much the same as the position of powered flight in 1900. A few people know that it is possible , and as I ...
Page 662
... flight profile . The addition of propulsion engine noise would raise the peak noise level during transition by about 2.5 PNdB , but the propulsion engine noise would not alter the general shape of the noise profile . The noise level ...
... flight profile . The addition of propulsion engine noise would raise the peak noise level during transition by about 2.5 PNdB , but the propulsion engine noise would not alter the general shape of the noise profile . The noise level ...
Page 716
... flight . Rate gyros are used to sense departures from equilibrium flight in roll , pitch and yaw . Since the pitch axis is more critical than the others , the SAS is dualised in the pitch channel ; further , the system includes an ...
... flight . Rate gyros are used to sense departures from equilibrium flight in roll , pitch and yaw . Since the pitch axis is more critical than the others , the SAS is dualised in the pitch channel ; further , the system includes an ...
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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