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Aeroacoustics of low mach number flows : fundamentals, analysis, and measurement

Aeroacoustics of low mach number flows : fundamentals, analysis, and measurement
紙図書
Stewart Glegg and William DevenportAcademic Pressc2017
全国の図書館
  • 件名Aeroacoustics Mach number Aerodynamic noise
  • 件名（識別子）Aeroacoustics Mach number Aerodynamic noise

High-lift flight tunnel [microform] : phase II report / David Lofftus, Thomas Lund, Donald Rote ; [prepared ... under purchase order L-8871] ([NASA contractor report] ; NASA/CR-2000-210653)

High-lift flight tunnel [microform] : phase II report / David Lofftus, Thomas Lund, Donald Rote ; [prepared ... under purchase order L-8871] ([NASA contractor report] ; NASA/CR-2000-210653)
マイクロ図書
2000<YCA-NAS 1.26:210653>
国立国会図書館
  • 件名Lift High reynolds number Mach number Wind tunnel tests Test facili...

Full flight envelope direct thrust measurement on a supersonic aircraft [microform] / Timothy R. Conners and Robert L. Sims (NASA/TM ; 1998-206560)

Full flight envelope direct thrust measurement on a supersonic aircraft [microform] / Timothy R. Conners and Robert L. Sims (NASA/TM ; 1998-206560)
マイクロ図書
1998<YCA-NAS 1.15:206560>
国立国会図書館
  • 件名F-15 aircraft Turbofan engines Supersonic aircraft Mach number

Flow quality and operational enhancements in the NASA Lewis 8- by 6-Foot Supersonic Wind Tunnel [microform] / E. Allen Arrington, Jose C. Gonsalez, and Edward A. Becks ([NASA contractor report] ; NASA/CR-1998-207930)

Flow quality and operational enhancements in the NASA Lewis 8- by 6-Foot Supersonic Wind Tunnel [microform] / E. Allen Arrington, Jose C. Gonsalez, and Edward A. Becks ([NASA contractor report] ; NASA/CR-1998-207930)
マイクロ図書
1998<YCA-NAS 1.26:207930>
国立国会図書館
  • 件名Wind tunnels Supersonic wind tunnels Measuring instruments Mach number Calibrating

On the propagation of small perturbations in two simple aeroelastic systems [microform] / Angelo Iollo, Manuel E. Salas (ICASE report ; no. 98-30) ([NASA contractor report] ; NASA/CR-1998-208457)

On the propagation of small perturbations in two simple aeroelastic systems [microform] / Angelo Iollo, Manuel E. Salas (ICASE report ; no. 98-30) ([NASA contractor report] ; NASA/CR-1998-208457)
マイクロ図書
1998<YCA-NAS 1.26:208457>
国立国会図書館
  • 件名...dynamic forces Mach number Acoustic emission

A fan concept to meet the 2017 noise goals [microform] / James H. Dittmar (NASA/TM ; 1998-208663)

A fan concept to meet the 2017 noise goals [microform] / James H. Dittmar (NASA/TM ; 1998-208663)
マイクロ図書
1998<YCA-NAS 1.15:208663>
国立国会図書館
  • 件名Noise reduction Aircraft noise Guide vanes Mach number Rotors Tip speed

Determination of sun angles for observations of shock waves on a transport aircraft [microform] / David F. Fisher ... [et al.] ([NASA technical memorandum] ; NASA/TM-1998-206551)

Determination of sun angles for observations of shock waves on a transport aircraft [microform] / David F. Fisher ... [et al.] ([NASA technical memorandum] ; NASA/TM-1998-206551)
マイクロ図書
1998<YCA-NAS 1.15:206551>
国立国会図書館
  • 件名Wings Shadowgraph photography L-1011 aircraft Elevation angle Mach number

NASA Glenn 1-by 1-foot supersonic wind tunnel user manual [microform] / Kirk D. Seablom ... [et al.] ([NASA technical memorandum] ; NASA/TM-1999-208478)

NASA Glenn 1-by 1-foot supersonic wind tunnel user manual [microform] / Kirk D. Seablom ... [et al.] ([NASA technical memorandum] ; NASA/TM-1999-208478)
マイクロ図書
1999<YCA-NAS 1.15:208478>
国立国会図書館
  • 件名Mach number Reynolds number Supersonic wi...

Development of a flush airdata sensing system on a sharp-nosed vehicle for flight at Mach 3 to 8 [microform] / Mark C. Davis ... [et al.] ([NASA technical memorandum] ; NASA/TM-2000-209017)

Development of a flush airdata sensing system on a sharp-nosed vehicle for flight at Mach 3 to 8 [microform] / Mark C. Davis ... [et al.] ([NASA technical memorandum] ; NASA/TM-2000-209017)
マイクロ図書
2000<YCA-NAS 1.15:209017>
国立国会図書館
  • 件名Mach number Research vehicles Supersonic ...

Progress in Favré-Reynolds stress closures for compressible flows [microform] / V. Adumitroaie, J.R. Ristorcelli, D.B. Taulbee (ICASE report ; no. 98-21) ([NASA contractor report] ; 2078423)

Progress in Favré-Reynolds stress closures for compressible flows [microform] / V. Adumitroaie, J.R. Ristorcelli, D.B. Taulbee (ICASE report ; no. 98-21) ([NASA contractor report] ; 2078423)
マイクロ図書
1998<YCA-NAS 1.26:208423>
国立国会図書館
  • 件名Mixing layers (Fluids) Reynolds stress Compressible flow Compressible boundary layer Mach number

Studies of shock wave interactions with homogeneous and isotropic turbulence [microform] / G. Briassulis ... [et al] ([NASA contractor report] ; NASA/CR-1998-206948)

Studies of shock wave interactions with homogeneous and isotropic turbulence [microform] / G. Briassulis ... [et al] ([NASA contractor report] ; NASA/CR-1998-206948)
マイクロ図書
1998<YCA-NAS 1.26:206948>
国立国会図書館
  • 件名...pressible flow Mach number

A correlation between flight-determined derivatives and wind-tunnel data for the X-24B research aircraft [microform] / Alex G. Sim (NASA technical memorandum ; 113084)

A correlation between flight-determined derivatives and wind-tunnel data for the X-24B research aircraft [microform] / Alex G. Sim (NASA technical memorandum ; 113084)
マイクロ図書
1997<YCA-NAS 1.15:113084>
国立国会図書館
  • 件名X-24 aircraft Research aircraft Mach number Angle of attack Aerodynamics

Consistent initial conditions for the DNS of compressible turbulence [microform] / J.R. Ristorcelli, G.A. Blaisdell (ICASE report ; no. 96-49) (NASA contractor report ; 201589)

Consistent initial conditions for the DNS of compressible turbulence [microform] / J.R. Ristorcelli, G.A. Blaisdell (ICASE report ; no. 96-49) (NASA contractor report ; 201589)
マイクロ図書
1996<YCA-NAS 1.26:201589>
国立国会図書館
  • 件名Compressibility effect Turbulent flow Mach number Computerized simulation Compr...

Impingement of boundary-reflected disturbances originating at the nose of a body of revolution in the Langley Research Center 16-foot transonic tunnel [microform] / Richard J. Re and Francis J. Capone (NASA/TM ; 1998-208723)

Impingement of boundary-reflected disturbances originating at the nose of a body of revolution in the Langley Research Center 16-foot transonic tunnel [microform] / Richard J. Re and Francis J. Capone (NASA/TM ; 1998-208723)
マイクロ図書
1998<YCA-NAS 1.15:208723>
国立国会図書館
  • 件名...re Shock waves Mach number Bow waves Bodies of revolutio...

Mach number effects on turbine blade transition length prediction [microform] / R.J. Boyle and F.F. Simon (NASA/TM ; 1998-208404)

Mach number effects on turbine blade transition length prediction [microform] / R.J. Boyle and F.F. Simon (NASA/TM ; 1998-208404)
マイクロ図書
1998<YCA-NAS 1.15:208404>
国立国会図書館
  • 件名Mach number Turbine blades Mathematical m...

Preconditioning for numerical simulation of low Mach number three-dimensional viscous turbomachinery flows [microform] / Daniel L. Tweedt and Rodrick V. Chima, Eli Turkel (NASA technical memorandum ; 113120)

Preconditioning for numerical simulation of low Mach number three-dimensional viscous turbomachinery flows [microform] / Daniel L. Tweedt and Rodrick V. Chima, Eli Turkel (NASA technical memorandum ; 113120)
マイクロ図書
1997<YCA-NAS 1.15:113120>
国立国会図書館
  • 件名Numerical analysis Mach number Three dimensional flow Turbom...

Experimental and theoretical study of flow fields around ducted-nacelle models [microform] / Robert J. Mack (NASA/TM ; 1998-207683)

Experimental and theoretical study of flow fields around ducted-nacelle models [microform] / Robert J. Mack (NASA/TM ; 1998-207683)
マイクロ図書
1998<YCA-NAS 1.15:207683>
国立国会図書館
  • 件名Nacelles Ducted flow Mach number Ducted bodies Flow characteri...

Porous and microporous honeycomb composites as potential boundary-layer bleed materials [microform] / D.O. Davis and B.P. Willis, M. Schoenenberger (NASA technical memorandum ; 113160)

Porous and microporous honeycomb composites as potential boundary-layer bleed materials [microform] / D.O. Davis and B.P. Willis, M. Schoenenberger (NASA technical memorandum ; 113160)
マイクロ図書
1997<YCA-NAS 1.15:113160>
国立国会図書館
  • 件名...site materials Mach number Boundary layer control Supers...

Experimental investigation of the flow field in a transonic, axial flow compressor, with respect to the development of blockage and loss / Kenneth L. Suder (NASA technical memorandum ; 107310)

Experimental investigation of the flow field in a transonic, axial flow compressor, with respect to the development of blockage and loss / Kenneth L. Suder (NASA technical memorandum ; 107310)
マイクロ図書
1996<YCA-NAS 1.15:107310>
国立国会図書館
  • 件名...rbocompressors Mach number Transonic compressors Shock w...

Numerical simulation of the generation of axisymmetric mode jet screech tones [microform] / H. Shen and C.K.W. Tam ([NASA contractor report] ; 207286)

Numerical simulation of the generation of axisymmetric mode jet screech tones [microform] / H. Shen and C.K.W. Tam ([NASA contractor report] ; 207286)
マイクロ図書
1998<YCA-NAS 1.26:207286>
国立国会図書館
  • 件名... Screech tones Mach number Aeroacoustics Axial flow Axia...