David E. Hahne

• Evaluation of the low-speed stability and control characteristics of a Mach 5.5 waverider concept
• Experimental and numerical optimization of a high-lift system to improve low-speed performance, stability, and control of an arrow-wing supersonic transport
• Full-scale semispan tests of a business-jet wing with a natural laminar flow airfoil
• Low-speed aerodynamic data for an 0.18-scale model of an F-16XL with various leading-edge modifications
• Low-speed static and dynamic force tests of a generic supersonic cruise fighter configuration
• Wind-tunnel free-flight investigation of a supersonic persistence fighter