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Wind-Tunnel Tests on a Series of Wing Models Through a Large Angle of Attack Range. Part I : Force Tests (1930)

NASA Technical Reports Server (NTRS) · leaf 14

An illustration from Wind-Tunnel Tests on a Series of Wing Models Through a Large Angle of Attack Range. Part I : Force Tests, 1930, leaf 14 — 13 WIND TUNNEL FORCE TESTS … 100 _4QO _2Qo qo 20o 4Q- 60" 80° T.L. a Figure 10.—Monoplane wings. Aspect ratio effect. Clark Y. Circular tips. 5-inch chord

NASA Technical Reports Server (NTRS)

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