Curves of lift, moment, and drag were determined up to Mach numbers of M=0.87, and are compared to rectangular wing. English translation from Lilienthal-Gesellschaft fuer Luftfahrtforschung, Report 156, p 30-40.
High-speed measurements on swept-back wing (Sweepback Angle phi=35°)
Nat Advisory Committee Aeronautics -- Tech Memo
1947
17 pages
16 Supp plates
Report
English
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Engineering Index Backfile | 1950
|Emerald Group Publishing | 1950
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