Wind Tunnel Tests of Elliptical Missile Body Configurations at Mach Numbers 0.4 to 0.5

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Report Number: AFWAL TR 87-3088
Author(s): Shereda, Donald E., Amidon, Paul F., Dahlem, Valentine, III
Corporate Author(s): High Speed Aero Performance Branch, Aeromechanics Division
Date of Publication: 1987-12
Pages: 161
DoD Task:
Identifier: ADA193525

Abstract:
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Provenance: Lockheed Martin Missiles & Fire Control

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