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A correlation by means of transonic similarity rules of experimentally determined characteristics of a series of symmetrical and cambered wings of rectangular plan form
Transonic similarity rules are applied to the correlation of experimental data for a series of related rectangular wings of varying aspect ratio, thickness, and camber. The data correlation is presented in two parts: the first part presents the correlation for a series of 22 wings having symmetrical NACA 63a-series sections; the second part is concerned with a study of one type of camber by correlation of the data for a series of 18 cambered wings having NACA 63a2xx and 63a4xx sections.
Date:
December 17, 1951
Creator:
McDevitt, John B.
System:
The UNT Digital Library
An investigation of four wings of square plan form at a Mach number of 6.9 in the Langley 11-inch hypersonic tunnel
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:
April 17, 1951
Creator:
McLellan, Charles H.; Bertram, Mitchel H. & Moore, John A.
System:
The UNT Digital Library