An investigation of four wings of square plan form at a Mach number of 6.86 in the Langley 11-inch hypersonic tunnel

Charles H. McLellan, Mitchel H. Bertram, John A. Moore
naca-rm-l51d17
Jun 1951


The results of pressure-distribution and force tests of four wings at a Mach number of 6.86 and a Reynolds number of 980,000 in the Langley 11-inch hypersonic tunnel are presented. The wings tested had a 4-inch square plan form, a 5-percent maximum thickness, with diamond, half-diamond, wedge, and half-circular-arc sections.

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