The Aeronautical Journal, Volume 73Royal Aeronautical Society, 1969 - Aeronautics |
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Page 607
... load in the direction of taper . An experimental investigation into the end load buckling problem for a plate having simply - supported edges with the sides pre- vented from moving normally in the plane of the plate is described in ref ...
... load in the direction of taper . An experimental investigation into the end load buckling problem for a plate having simply - supported edges with the sides pre- vented from moving normally in the plane of the plate is described in ref ...
Page 608
... LOAD ESTIMATED EXPERIMENTAL BUCKLING LOAD -ESTIMATED EXPERIMENTAL BUCKLING LOAD 1-0 02 04 06 08 10 WHERE - DISTANCE ALONG PLATE LONGITUDINAL BUCKLED SHAPE - COMPARISON WITH EXACT RESULT ( SINE ) 1.0 0.5 PLATE NO 2 9 -2 21 . - 2 0 POPES ...
... LOAD ESTIMATED EXPERIMENTAL BUCKLING LOAD -ESTIMATED EXPERIMENTAL BUCKLING LOAD 1-0 02 04 06 08 10 WHERE - DISTANCE ALONG PLATE LONGITUDINAL BUCKLED SHAPE - COMPARISON WITH EXACT RESULT ( SINE ) 1.0 0.5 PLATE NO 2 9 -2 21 . - 2 0 POPES ...
Page 893
Effects of Solid Viscosities , Loading Velocities and Initial Deflections to Dynamic Buckling Loads of a Column SHIN ... load for these cases can easily be found from expression 7 since , for the simply - supported case , the minimum ...
Effects of Solid Viscosities , Loading Velocities and Initial Deflections to Dynamic Buckling Loads of a Column SHIN ... load for these cases can easily be found from expression 7 since , for the simply - supported case , the minimum ...
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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