Slender cone boundary layer transition under angle of attack at Mach 21 with promoted leeward and fixed windward ray
Effect of angle of attack on boundary-layer transition at Mach 21
01.06.1971
Sonstige
Keine Angabe
Englisch
BOUNDARY-LAYER TRANSITION ON CONES AT ANGLE OF ATTACK IN A MACH-6 QUIET TUNNEL
British Library Conference Proceedings | 2010
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