A Wind-Tunnel Investigation of the Aerodynamic Characteristics of Bodies of Revolution at Mach Numbers of 2.37, 2.98, AND 3.90 at Angles of Attack to 90 Deg
1960
36 pages
Report
No indication
English
Aerodynamic characteristics , Nose cone , Supersonic speed , Supersonic wind tunnel , Aerodynamics , Body , Characteristics , Cone , Configuration , Drag , Force , High angle , Nose , Revolution , Speed , Supersonic , Testing , Tunnel , Wind