Henry T. Nagamatsu

• Aeroacoustics, acoustic wave propagation, aircraft noise prediction, aeroacoustic instrumentation
• Aeroacoustics, STOL noise, airframe and airfoil noise
• Computational, theoretical, and experimental investigation of flow over a sharp flat plate, M1 = 10 - 25
• Heat transfer on a flat plate in continuum to rarefied hypersonic flows at Mach numbers of 19.2 and 25.4
• Hypersonic nozzle expansion with air atom recombination present
• Investigation to optimize the passive shock wave/boundary layer control for supercritical airfoil drag reduction
• Real gas effects in flow over blunt bodies at hypersonic speeds
• Shock tube technology and design