Factors relating to power plant problem for high speed aircraft concentrating mainly on problem of wing planforms and overall aircraft configurations for Mach number range of 0 to 2; thin, straight wing best up to Mach 2; delta or swept designs do not match lift or handling features of straight wing. (see also Aviation Week n 23 Dec 7 1953 p 26, 28, 31, 33-4, 37)
Airplane configurations for high speed flight
Soc Automotive Engrs -- Paper
Society of Automotive Engineers -- Meeting ; 1953 Design
1953
16 pages
Conference paper
English
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Airplane configurations for high speed flight
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