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

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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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
Language: en
Pages: 30
Authors: Robert L. Trimpi
Categories: Aerodynamic heating
Type: BOOK - Published: 1961 - Publisher:

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The temperature time history of various components of a 20-millimeter projectile was obtained by transient heating tests in a Mach number 5 blowdown tunnel. An
NASA Technical Note
Language: en
Pages: 384
Authors:
Categories:
Type: BOOK - Published: 1961 - Publisher:

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Bibliography of Scientific and Industrial Reports
Language: en
Pages: 1048
Authors:
Categories: Science
Type: BOOK - Published: 1961 - Publisher:

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Index of NASA Technical Publications
Language: en
Pages: 448
Authors: United States. National Aeronautics and Space Administration
Categories: Aeronautics
Type: BOOK - Published: 1960 - Publisher:

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