Lift and drag measurements made on models in Langley Unitary Plan wind tunnel; values of maximum lift-drag ratio were about 1.4 at Mach 2.65 and about 1.2 at Mach 4.65; angles of attack of tests were limited by unsteady behavior of models.
Wind-tunnel investigation of paraglider models at supersonic speeds
NASA -- Tech Notes
1961
16 pages
Report
English
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Wind Tunnel Investigation of a Rigid Paraglider Reference Wing
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