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