Wind tunnel investigation of hypersonic transport model aerodynamic characteristics at Mach numbers to 6 - graphs
Investigation of the aerodynamic characteristics of a hypersonic transport model at Mach numbers to 6
1971-04-01
Sonstige
Keine Angabe
Englisch
Shock tunnel study of spiked aerodynamic bodies flying at hypersonic Mach numbers
Tema Archiv | 2002
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