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Span Load Distribution on Two Monoplanes Wing Models as Affected by Twist and Sweepback (1930)
NASA Technical Reports Server (NTRS) · leaf 15
N.A.C.A. Technical Note No.346 Fig.6 Effect of sweep on N.A.C.A.86 semispan Fig.6 load distribution.NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
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