Wind-tunnel tests of a Clark Y wing with a narrow auxiliary airfoil in different positions (1933)
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541 WIND-TUNNEL TESTS Off A CLARK T "WTNG II I I I I I I I IX) • Plain Clark Y- I.O 2.0 a 6~+5° 6"- 5° + x +Z5° --15° v- □ 0° "-25° … a, degrees a, degrees Figure ll.—Characteristics of combination of main and auxiliary wings with Fiqxtbe 10.—Characteristics of combination of main and auxiliary wings with trailing edge of auxiliary 10 per cent obord ahead of leading edge and 15 per cent trailing edge of auxiliary 10 per cent…
NASA Technical Reports Server (NTRS)
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