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Chapter I Strength Requirements
Main Plane Loads and Forces
Design of Main Planes
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aerofoil aeroplane aileron air flow aircraft angle of attack aspect ratio assumed attached auto-towing axis bending bolts British Gliding Association bulkheads cable calculated cantilever centre of pressure chord coefficient connected construction control surfaces curve decreases distance dive Duralumin dynamic soaring elevator employed factor fittings flanges flying front spar fuselage glider Gottingen 535 ground hill hinge horizontal increased induced drag joint king-post landing launching lbs./sq leading edge length lift coefficient load diagram longerons lugs machine main plane main spar maximum method monocoque normal nose obtained owing pilot plywood position pulley rear spar rudder sailplane shape shear shear stress shown in Fig slots soaring flight span speed spruce stalling steel strength stress suitable tail load tail unit taper tension timber tips torsion torsional load towing trailing edge up-currents values velocity vertical whilst wind wing section wing weight wing-tip