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henry t nagamatsu

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Cilt sonuçları

Aeroacoustics, STOL noise, airframe and airfoil noise

Ira R. Schwartz, Henry T. Nagamatsu · Amer Inst of Aeronautics &

445 sayfa · 1976

Jet planes / Noise / Congresses

Aeroacoustics, acoustic wave propagation, aircraft noise prediction, aeroacoustic instrumentation

Schwartz Ira R., Henry T. Nagamatsu, Warren C. Strahle · American Institute of Aeronautics and Astronautics

307 sayfa · 1978

Airplanes / Noise / Congresses

TransmissionHeat transfer on a flat plate in continuum to rarefied hypersonic flows at Mach numbers of 19.2 and 25.4Henry T. Nagamatsu

Heat transfer on a flat plate in continuum to rarefied hypersonic flows at Mach numbers of 19.2 and 25.4

Henry T. Nagamatsu · National Aeronautics and Space Administration; [for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va.]

45 sayfa · 1970

Heat / Hypersonic wind tunnels / Rarefied gas dynamics / Transmission

Shock-boundary layer interactionComputational, theoretical, and experimental investigation of flow over a sharp flat plate, M1 = 10 - 25Henry T. Nagamatsu

Computational, theoretical, and experimental investigation of flow over a sharp flat plate, M1 = 10 - 25

Henry T. Nagamatsu · American Institute of Aeronautics and Astronautics

14 sayfa · 1994

Hypersonic flow / Shock-boundary layer interaction

CiltHypersonic nozzle expansion with air atom recombination presentHenry T. Nagamatsu

Hypersonic nozzle expansion with air atom recombination present

Henry T. Nagamatsu · General Electric, Research Laboratory

14 sayfa · 1960

Kategori yok

CiltShock tube technology and designHenry T. Nagamatsu

Shock tube technology and design

Henry T. Nagamatsu · General Electric, Research Laboratory

57 sayfa · 1958

Kategori yok

CiltReal gas effects in flow over blunt bodies at hypersonic speedsHenry T. Nagamatsu

Real gas effects in flow over blunt bodies at hypersonic speeds

Henry T. Nagamatsu · General Electric Research Laboratory

30 sayfa · 1959

Kategori yok

Boundary layer controlInvestigation to optimize the passive shock wave/boundary layer control for supercritical airfoil drag reductionHenry T. Nagamatsu

Investigation to optimize the passive shock wave/boundary layer control for supercritical airfoil drag reduction

Henry T. Nagamatsu · National Aeronautics and Space Administration, Langley Research Center

Sayfa sayısı yok · 1984

Aerofoils / Boundary layer control

Science/MathematicsAeroacoustics: Jet and Combustion Noise Henry T. Nagamatsu, Jack V. O'Keefe

Aeroacoustics: Jet and Combustion Noise

Henry T. Nagamatsu, Jack V. O'Keefe · Amer Inst of Aeronautics &

Sayfa sayısı yok · 1975

Science/Mathematics