Description: Report presenting an investigation in the transonic tunnel to determine the aerodynamic loading characteristics of a 3-percent-thick, aspect-ratio-2.06, 60 degree delta-wing-body combination at a range of Mach numbers and angles of attack. Results regarding pressure distributions, spanwise loadings, integrated wing coefficients, and tabulated pressure coefficients are provided.
Date: May 28, 1957
Creator: Swihart, John M. & Foss, Willard E., Jr.
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department