SShock tube technology and designShock tube technology and designde Henry T. NagamatsuEdiciones (1)Shock tube technology and design (1958)General Electric, Research LaboratoryMás obras de Henry T. NagamatsuAeroacoustics, STOL noise, airframe and airfoil noiseAeroacoustics, acoustic wave propagation, aircraft noise prediction, aeroacoustic instrumentationCComputational, theoretical, and experimental investigation oComputational, theoretical, and experimental investigation of flow over a sharp flat plate, M1 = 10 - 25
CComputational, theoretical, and experimental investigation oComputational, theoretical, and experimental investigation of flow over a sharp flat plate, M1 = 10 - 25
HHeat transfer on a flat plate in continuum to rarefied hyperHeat transfer on a flat plate in continuum to rarefied hypersonic flows at Mach numbers of 19.2 and 25.4
HHypersonic nozzle expansion with air atom recombination presHypersonic nozzle expansion with air atom recombination present
IInvestigation to optimize the passive shock wave/boundary laInvestigation to optimize the passive shock wave/boundary layer control for supercritical airfoil drag reduction
