Study made to determine transonic and supersonic longitudinal stability, control and drag characteristics of aircraft and missile configurations; from results obtained total effects of wing can be determined; for some of aerodynamic derivatives separate effects of wing, tail, and fuselage were determined.
Wing-on and wing-off longitudinal characteristics of airplane configuration having thin unswept wing of aspect ratio 3, as obtained from rocket-propelled models at mach numbers from 0.8 to 1.4
NASA -- Tech Note
1960
42 pages
Report
English
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