The Aeronautical Journal, Volume 73Royal Aeronautical Society, 1969 - Aeronautics |
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Page 714
... wing to provide the function of the collective pitch control of the helicopter , and in addition a very responsive ... wing loading at design gross weight is about 45 lb / sq ft . The disc loading based on total disc area is about 30 lb ...
... wing to provide the function of the collective pitch control of the helicopter , and in addition a very responsive ... wing loading at design gross weight is about 45 lb / sq ft . The disc loading based on total disc area is about 30 lb ...
Page 723
... wing drag is not as effective as one might expect . In larger or in tandem - seat aircraft designs , reduction in wing size is more profitable , and we would then use an extendable - chord wing to preserve the good low - speed ...
... wing drag is not as effective as one might expect . In larger or in tandem - seat aircraft designs , reduction in wing size is more profitable , and we would then use an extendable - chord wing to preserve the good low - speed ...
Page 947
... Wing sections . Figure 8. The Trident 1E leading edge . TRIDENT 36 38 AN INCREASE OF 9 % Fuselage The fuselage ... wing front spar , and 96 in ( 2.4 m ) aft of the wing . A Trident 1 type galley loading door is provided on the starboard ...
... Wing sections . Figure 8. The Trident 1E leading edge . TRIDENT 36 38 AN INCREASE OF 9 % Fuselage The fuselage ... wing front spar , and 96 in ( 2.4 m ) aft of the wing . A Trident 1 type galley loading door is provided on the starboard ...
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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