Transonic and Supersonic Flutter Trend Investigation of a Variable-sweep Wing
Transonic and Supersonic Flutter Trend Investigation of a Variable-Sweep Wing
Transonic Flutter Investigation of Models of a Proposed Variable-Sweep Wing
Aerodynamic Characteristics of an Ogee-Wing Space Shuttle Orbiter Concept at a Mach Number of 2.01
The Longitudinal Stability Characteristics of an Ogee Wing of Slenderness Ratio Equals 0.35
Low-Speed Wind Tunnel Tests of 1/9-Scale Model of a Variable-Sweep Supersonic Cruise Aircraft