Theoretical mathematical study of wave resistance of airfoils at supersonic velocity leading to conclusion that sections used must be considerably more tapered than formerly; tip effect drag; small wing areas and small angles of incidence must be accepted. Before Fifth Volta Conference, Rome, 1935.
Aerodynamischer Auftrieb bei Ueberschallgeschwindigkeit
Aerodynamischer Auftrieb bei Ueberschallgeschwindigkeit
Luftfahrtforschung ; 12 , n 6
1935
11 pages
Bibliography
Article (Journal)
German
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Tragfluegeltheorie bei Ueberschallgeschwindigkeit
Engineering Index Backfile | 1936
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