Heat Transfer Tests Of 20 Millimeter Projectiles At A Mach Number Of 5 With An Analysis By Unsteady Scaling Laws To Predict Component Temperature Rises After Firing For Various Free Flight Conditions
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Heat-transfer Tests of 20-millimeter Projectiles at a Mach Number of 5 with an Analysis by Unsteady Scaling Laws to Predict Component Temperature Rises After Firing for Various Free-flight Conditions
Author | : Robert L. Trimpi |
Publisher | : |
Total Pages | : 36 |
Release | : 1961 |
Genre | : Aerodynamic heating |
ISBN | : |
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