Wind Tunnel Tests of Elliptical Missile Body Configurations at Mach Numbers 0.4 to 0.5
This report has yet to be scanned by Contrails staff
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:
The abstract for this report is either unavailable or has yet to be entered
Provenance: Lockheed Martin Missiles & Fire Control
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:
The abstract for this report is either unavailable or has yet to be entered
Provenance: Lockheed Martin Missiles & Fire Control