Problems discussed refer specifically to convertaplane, Model HV-2A, which has flying characteristics of both rotor plane and conventional airplane; conversion accomplished by releasing and starting upper wing rotating and by control of its unbalanced moments, occasioned by differential in lift between advancing and receding blades of rotor wing. Before Inst Aeronautical Sciences.
Some aerodynamic problems in design of convertible airplane
J Aeronautical Sciences
Journal of Aeronautical Sciences ; 5 , n 12
1938
4 pages
Article (Journal)
English
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Some aerodynamic problems in design of convertible airplane
Engineering Index Backfile | 1938
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