Investigation of Aerodynamic Characteristics of an Airplane Configuration Having Tail Surfaces Outboard of the Wing Tips at Mach Numbers of 2.30, 2.97, AND 3.51
1958
52 pages
Report
Keine Angabe
Englisch
Aerodynamic characteristics , Aircraft configuration , Supersonic speed , Tail surface , Wind tunnel stability test , Wing tip , Aerodynamic , Aircraft , Characteristics , Configuration , Drag , Outboard , Reynolds number , Speed , Stability , Supersonic , Surface , Tail , Test , Tip , Trim , Tunnel , Wind , Wing