The Aeronautical Journal, Volume 73Royal Aeronautical Society, 1969 - Aeronautics |
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Page 700
... response of a slender aircraft to rudder . divergence and the faster will be the consequent auto- rotation . The problem becomes increasingly serious with increasing negative normal acceleration . The mere fact that an aircraft can ...
... response of a slender aircraft to rudder . divergence and the faster will be the consequent auto- rotation . The problem becomes increasingly serious with increasing negative normal acceleration . The mere fact that an aircraft can ...
Page 971
... response G ( s ) included . ( b ) Zero structural damping engine response G ( s ) included . ( c ) Zero structural damping , engine response excluded G ( s ) = 1. ( d ) Zero structural damping , engine response excluded G ( s ) = 1 ...
... response G ( s ) included . ( b ) Zero structural damping engine response G ( s ) included . ( c ) Zero structural damping , engine response excluded G ( s ) = 1. ( d ) Zero structural damping , engine response excluded G ( s ) = 1 ...
Page 1047
... response of linear systems but the method most often used in the study of structures is the steady state vector response method " , the natural frequencies and damping ratios being measured from the resulting vector diagrams . This ...
... response of linear systems but the method most often used in the study of structures is the steady state vector response method " , the natural frequencies and damping ratios being measured from the resulting vector diagrams . This ...
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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