Investigation of basic relationships which are involved in aim of obtaining further improvements; project calculations with respect to power, wing section and area; layout of design; flying characteristics and stability and control; it is concluded that laminar flow airfoil sections with built-in camber simulating small flap angle appear to be best.
Design philosophy of man powered aircraft
Roy Aeronautical Soc -- J
Royal Aeronautical Society -- Journal ; 66 , n 623
1962
8 pages
Aufsatz (Zeitschrift)
Englisch
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