Consideration of friction, form and induced drag of wings and friction and form drag of fuselage and tail unit, with view to possibilities which exist to improve aircraft performance. English abstract from Flugwehr u Technik July 1942.
Drag problems in present day aircraft design
Engrs' Digest
Engineers' Digest ; 111 , n 12
1942
4 pages
Aufsatz (Zeitschrift)
Englisch
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