The Aeronautical Journal, Volume 73Royal Aeronautical Society, 1969 - Aeronautics |
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Page 593
... given load system or load envelope , and this has been treated by Harris ( " ) for planar load envelopes bounded by given values of applied stresses σr , σ and Tay . Here we consider a problem of optimum fibre arrangement to transfer a ...
... given load system or load envelope , and this has been treated by Harris ( " ) for planar load envelopes bounded by given values of applied stresses σr , σ and Tay . Here we consider a problem of optimum fibre arrangement to transfer a ...
Page 802
... given of the power required for a supersonic tunnel . There is also a brief discussion of wind tunnel corrections , with a number of references to research reports . The next chapter deals with apparatus for measuring velocity and ...
... given of the power required for a supersonic tunnel . There is also a brief discussion of wind tunnel corrections , with a number of references to research reports . The next chapter deals with apparatus for measuring velocity and ...
Page 911
... given in terms of a and e by eqn . ( 9 ) . We now have enough parameters to describe the subse- quent motion completely , assuming this motion takes place . in the same plane as the Earth's orbit . TRANSFER BETWEEN CIRCULAR ORBITS To ...
... given in terms of a and e by eqn . ( 9 ) . We now have enough parameters to describe the subse- quent motion completely , assuming this motion takes place . in the same plane as the Earth's orbit . TRANSFER BETWEEN CIRCULAR ORBITS To ...
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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