An aircraft is presented. The aircraft comprises a tow point positioned on a body of the aircraft and forward of main landing gear of the aircraft, wherein the tow point is connected to an airframe of the aircraft to accept and distribute forces forward, aft, and normal to the aircraft.
AIRCRAFT TOW POINT
2021-01-21
Patent
Electronic Resource
English
Aircraft Control Using Stagnation Point Displacement
British Library Conference Proceedings | 1997
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