An investigation of four wings of square plan form at a Mach number of 6.9 in the Langley 11-inch hypersonic tunnel
Description: The results of pressure-distribution and force tests of four wings at a Mach number of about 6.9 and a Reynolds number of 0.98 x 10(6) in the Langley 11-inch hypersonic tunnel are presented. The wings had a square plan form, a 5-percent-chord maximum thickness, and diamond, half-diamond, wedge, and half-circular sections.
Date: January 1, 1957
Creator: Mclellan, Charles H; Bertram, Mitchel H & Moore, John A
Item Type: Report
Partner: UNT Libraries Government Documents Department