Effect of angle of attack on boundary-layer transition at Mach 21
FISCHER, M. C., RUDY, D. H. /NASA, LANGLEY RESEARCH CENTER, HYPERSONIC VEHICLES DIV., HAMPTON, VA./.
AIAA Journal ; 9 , 6 ; 1203-1205
1971
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
BOUNDARY-LAYER TRANSITION ON CONES AT ANGLE OF ATTACK IN A MACH-6 QUIET TUNNEL
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