Some Measurements of the Buffet Region of a Swept-wing Research Airplane During Flights to Supersonic Mach Numbers (1953)
NASA Technical Reports Server (NTRS) · leaf 12
CONFIDENTIAL ’ -30 .82 .84 .86 .88 .90 .92 .94 .96 .98 1.00 1.02 M Figure 3.- Variation of airplane normal-force coefficient and buffet intensity with Mach number during a rocket-powered climb. I I
NASA Technical Reports Server (NTRS)
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