Aerodynamic characteristics of the hemisphere at supersonic and hypersonic Mach numbers.
CLARK, E. L. /SANDIA CORP., SANDIA LAB., EXPERIMENTAL AERODYNAMICS DIV., ALBUQUERQUE, N. MEX./.
AIAA Journal ; 7 , 7 ; 1385-1386
1969-01-01
2 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Shock tunnel study of spiked aerodynamic bodies flying at hypersonic Mach numbers
Tema Archiv | 2002
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