Wind tunnel study made to determine aerodynamic loading characteristics at 0.80 to 1.05 Mach and at angles of attack to 26°; pressure distributions and tabulated pressure coefficients are presented; leading edge separation vortex is dominant flow-field phenomenon.
Transonic load characteristics of 3-percent-thick 60° delta-wing-body combination
NASA -- Tech Note
1961
127 pages
Report
English
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