Mathematical analysis of mechanical characteristics of orthoplane class of aircraft, including helicopters; mathematical proof of proposition that hovering aircraft cannot exert dynamic lift exceeding its propeller thrust and that traveling airplane supports about same gross weight, per unit thrust, with its wings inside as with them outside propeller wash; practicability of orthoplanes.
Orthoplane theorems
J Aeronautical Sciences
Journal of Aeronautical Sciences ; 3 , n 9
1936
2 pages
Aufsatz (Zeitschrift)
Englisch
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