Force tests on a proposed body shape of the Hermes A-2 missile with and without longitudinal spoilers were made at Mach number 4.04. Values of normal force coefficient, pitching-moment coefficient, and center-of-pressure position were obtained.
Tests of a Hermes A-2 Missile Body at Mach Number 4.04
1950-01-01
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
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