Free-flight Range Tests of Spinning Tubular Projectiles at Mach Numbers from 2.0 to 3.2

Free-flight Range Tests of Spinning Tubular Projectiles at Mach Numbers from 2.0 to 3.2
Author: G. L. Winchenback
Publisher:
Total Pages: 54
Release: 1979
Genre: Ballistic ranges
ISBN:
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Free-flight Range Tests of Spinning Tubular Projectiles at Mach Numbers from 2.0 to 3.2
Language: en
Pages: 54

Free-flight Range Tests of Spinning Tubular Projectiles at Mach Numbers from 2.0 to 3.2

Authors: G. L. Winchenback
Categories: Ballistic ranges
Type: BOOK - Published: 1979 - Publisher:

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Aerodynamic Testing in a Free-flight Spark Range
Language: en
Pages: 172

Aerodynamic Testing in a Free-flight Spark Range

Authors: G. L. Winchenbach
Categories: Aerodynamics
Type: BOOK - Published: 1997 - Publisher:

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Free Flight Range Test of the Improved 20-millimeter Target Practice Round (PJU-5/B)
Language: en
Pages: 38

Free Flight Range Test of the Improved 20-millimeter Target Practice Round (PJU-5/B)

Authors: Kenneth K. Cobb
Categories: Ballistic ranges
Type: BOOK - Published: 1979 - Publisher:

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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: 36

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

Authors: Robert L. Trimpi
Categories: Aerodynamic heating
Type: BOOK - Published: 1961 - Publisher:

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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

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

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