Flying at very high speeds results in excessive resistance, surface heating, and indeterminate character of flow at Mach numbers between 0.85 and 1.2; analysis of types of airfoils that will be needed, powers required and what must be done to overcome problems of friction and extremely high altitude heating effects; new problems of high altitude flight are ionization of air, meteoric dust, and electrification of atmosphere. (See also - n 11 Nov 1945 p 131-4)
Analyzing aspects of future flight
Aviation
Aviation ; 44 , n 12 ; p 158-162
1945
5 pages
Bibliography
Article (Journal)
English
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