William P. Henderson

• Aerodynamic characteristics of a tandem wing configuration at a mach number of 0.30
• Broken Heart
• Effect of empennage arrangement on single engine nozzle/afterbody static pressures at transonic speeds
• Effects of wing leading-edge flap deflections on subsonic longitudinal aerodynamic characteristics of a wing-fuselage configuration with a 44 ̊swept wing
• Stability and control characteristics of a three-surface advanced fighter configuration at angles of attack up to 45⁰