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Wind Tunnel Tests of Elliptical Missile Body Configurations at Mach Numbers 0.4 to 0.5
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
Report number: AFWAL TR 87-3088

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