United States. National Advisory Committee for Aeronautics. (1937). Full-scale span load distribution on tapered wing with split flaps of various spans. [s.n.].
Chicago Style (17th ed.) CitationUnited States. National Advisory Committee for Aeronautics. Full-scale Span Load Distribution on Tapered Wing with Split Flaps of Various Spans. [Washington]: [s.n.], 1937.
MLA (9th ed.) CitationUnited States. National Advisory Committee for Aeronautics. Full-scale Span Load Distribution on Tapered Wing with Split Flaps of Various Spans. [s.n.], 1937.
Warning: These citations may not always be 100% accurate.