Pressure distributions on 3 rigid wings simulating parawings with varied canopy curvature and leading edge sweep at mach 2.29 to 4.65
PRESSURE DISTRIBUTIONS ON THREE RIGID WINGS SIMULATING PARAWINGS WITH VARIED CANOPY CURVATURE AND LEADING-EDGE SWEEP AT MACH NUMBERS FROM 2.29 TO 4.65
1963-04-01
Sonstige
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Englisch