Results of analysis illustrated by graphs showing comparative effectiveness of different methods of increasing flying speed; high wing loading presents greatest need for higher speeds at sea level; optimum wing loading for maximum flying speed shown to be that required to fly at maximum L/D of wing and tail surfaces. Before Inst Aeronautical Sciences.
Some problems in design of high-speed aircraft
J Aeronautical Sciences
Journal of Aeronautical Sciences ; 5 , n 7
1938
5 pages
Article (Journal)
English
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Some problems in design of high-speed aircraft
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