Stability and Control Characteristics at a Mach Number of 1.97 of an Airplane Configuration Having Two Types of Variable- Sweep Wings
1960
48 pages
Report
No indication
English
Avionics , Aerodynamic stability , Supersonic wind tunnel , Variable sweep , Aerodynamic , Angle , Chord , Control , Geometry , Lift , Mach number , Pitch , Pivot , Stability , Supersonic , Sweep , Tunnel , Variable , Wind , Wing