Force tests on monoplane and biplane wing models with angle of attack from minus 45 to plus 90 deg. were conducted in Langley atmospheric wind tunnel; tests were to determine effects of variations of tip shape, aspect ratio, flap setting, stagger, gap, decalage, sweep back, and airfoil profile; effects produced given in preliminary form by comparative curves.
Wind tunnel force tests in wing systems through large angles of attack
Nat. Advisory Committee Aeronautics -- Tech. Note
1928
7 pages
19 Figs.
Report
English
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Wind tunnel tests on a series of wing models through a large angle of attack range
Engineering Index Backfile | 1929
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