Minimum Drag of Four Versions of a Swept-Wing Fighter Airplane Obtained from Flight Tests of Rocket-Boosted Models at Mach Numbers from 0.81 to 1.71
1956
32 pages
Report
No indication
English
Aeronautics , Aircraft configuration , Drag coefficient , Fighter aircraft , Swept wing , Aircraft , Area , Coefficient , Configuration , Cross section , Drag , External , Fighter , Forebody , Mach number , Reduction , Sweep , Test , Wing