Effects of Sweep and Angle of Attack on Boundary-layer Transition on Wings at Mach Number 4.04
01.08.1955
Sonstige
Keine Angabe
Englisch
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
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