Analysis of Relaxed Static Stability and Maneuver Load Control Applications to a Large Bomber
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
Evaluation of an Aeroelastic Model Technique for Predicting Airplane Buffet Loads
Dual-Fuselage Aircraft Having Yawable Wing and Horizontal Stabilizer
Low-Speed Wind Tunnel Tests of 1/9-Scale Model of a Variable-Sweep Supersonic Cruise Aircraft
Wind Tunnel Experiments on an Actively Controlled, Variable Geometry Flutter Model
Determining Parameters of Aircraft with Variable-Sweep Wing