Modifications to model such as changes in fuselage shape, leading edge extensions on wing, special wing bodies, and lower surface ridges on wing were investigated to determine effects on longitudinal stability and maximum lift-drag ratio; Mach number range from 0.40 to 0.96 was covered.
Longitudinal aerodynamic characteristics of high-subsonic-speed transport airplane model with cambered 40° sweptback wing of aspect ratio 8 at Mach numbers to 0.96
NASA -- Tech Note
1960
88 pages
Report
Englisch
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