Effects of sweep and angle of attack on boundary-layer transition on wings at Mach number 4.04
1955
31 S
Ill., graph. Darst
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Effects of sweep and angle of attack on boundary-layer transition on wings at mach number 4.04
Engineering Index Backfile | 1955
|Tests of a Hermes A-2 Missile Body at Mach Number 4.04
NTRS | 1950
|