An investigation of four wings of square plan form at a Mach number of 6.86 in the Langley 11-inch hypersonic tunnel
Description: Report presenting the results of pressure-distribution and force tests on four wings at Mach number 6.86 and Reynolds number 980,000 in the 11-inch hypersonic tunnel. Characteristics of the wings tested included a 4-inch square plan form, a 5-percent maximum thickness, and diamond, half-diamond, wedge, and half-circular-arc sections. Information about pressure measurements, wing characteristics, and Schlieren photographs is provided.
Date: June 29, 1951
Creator: McLellan, Charles H.; Bertram, Mitchel H. & Moore, John A.
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department