The Aeronautical Journal, Volume 73Royal Aeronautical Society, 1969 - Aeronautics |
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Page 598
... associated displacement vector PNB is conveniently written PNB = { U1 U1 , a U1 , aa U2 U1⁄2 , a U1⁄2 , aa V1 V1 , a ... associated with the vector pw of the third eqn . ( 9 ) , as where N E Jow = 6 [ PONTENON Ν Ω ( 21 × 1 ) ( 53 ) is ...
... associated displacement vector PNB is conveniently written PNB = { U1 U1 , a U1 , aa U2 U1⁄2 , a U1⁄2 , aa V1 V1 , a ... associated with the vector pw of the third eqn . ( 9 ) , as where N E Jow = 6 [ PONTENON Ν Ω ( 21 × 1 ) ( 53 ) is ...
Page 600
... associated with freedoms incor- porating first derivatives with respect to a and y must be reversed . Our remarks in ref . 1 concerning the rotational degrees of freedom at the intermediate nodal points are , of course , also applicable ...
... associated with freedoms incor- porating first derivatives with respect to a and y must be reversed . Our remarks in ref . 1 concerning the rotational degrees of freedom at the intermediate nodal points are , of course , also applicable ...
Page 829
... associated with Air Transport for at least 10 years . Age limits 35/45 years of age . Special consideration may be given to serving officers under 50 in the R.N. , R.A.F. and the Army Air Corps . a The Company considers this position ...
... associated with Air Transport for at least 10 years . Age limits 35/45 years of age . Special consideration may be given to serving officers under 50 in the R.N. , R.A.F. and the Army Air Corps . a The Company considers this position ...
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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