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Pratt & Whitney/Boeing engine validation of noise reduction concepts : final report for NASA contract NAS3-97144 . phase 1 / / Douglas C. Mathews [and six others]
| Pratt & Whitney/Boeing engine validation of noise reduction concepts : final report for NASA contract NAS3-97144 . phase 1 / / Douglas C. Mathews [and six others] |
| Autore | Mathews Douglas C. |
| Pubbl/distr/stampa | East Hartford, Connecticut : , : United Technologies Corporation, Pratt & Whitney |
| Descrizione fisica | 1 online resource (vi, 139 pages) : color illustrations |
| Collana | NASA/CR |
| Soggetto topico |
Nose inlets
Supersonic flow Impedance measurement Flow resistance Navier-Stokes equation Boundary layer thickness |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Pratt & Whitney/Boeing engine validation of noise reduction concepts |
| Record Nr. | UNINA-9910702672103321 |
Mathews Douglas C.
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| East Hartford, Connecticut : , : United Technologies Corporation, Pratt & Whitney | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Seeding for laser velocimetry in confined supersonic flows with shocks / / J. Lepicovsky and RJ. Bruckner
| Seeding for laser velocimetry in confined supersonic flows with shocks / / J. Lepicovsky and RJ. Bruckner |
| Autore | Lepicovsky Jan |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , July 1996 |
| Descrizione fisica | 1 online resource (9 pages) : illustrations |
| Collana | NASA technical memorandum |
| Soggetto topico |
Laser doppler velocimeters
Reliability Supersonic flow Optical measuring instruments Velocity measurement |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910707356503321 |
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Lepicovsky Jan
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , July 1996 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Study of injection of helium into supersonic air flow using Rayleigh scattering / / Richard G. Seasholtz and Alvin E. Buggele
| Study of injection of helium into supersonic air flow using Rayleigh scattering / / Richard G. Seasholtz and Alvin E. Buggele |
| Autore | Seasholtz Richard G. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , January 1997 |
| Descrizione fisica | 1 online resource (12 pages) : illustrations |
| Collana | NASA technical memorandum |
| Soggetto topico |
Rayleigh scattering
Supersonic flow Air flow Gas injection Helium Cross flow YAG lasers Pulsed lasers Flow visualization |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910707631603321 |
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Seasholtz Richard G.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , January 1997 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Use of hyperbolic grid generation scheme in simulating supersonic viscous flow about three-dimensional winged configurations / Yehia M. Rizk, Joseph L. Steger, Denny S. Chausse
| Use of hyperbolic grid generation scheme in simulating supersonic viscous flow about three-dimensional winged configurations / Yehia M. Rizk, Joseph L. Steger, Denny S. Chausse |
| Autore | Rizk Yehia M. |
| Pubbl/distr/stampa | Moffett Field, CA : , : National Aeronautics and Space Administration, Ames Research Center, , July 1985 |
| Descrizione fisica | 1 online resource (13 pages) : illustrations |
| Collana | NASA technical memorandum |
| Soggetto topico |
Computational grids
Grid generation (mathematics) Space Shuttle orbiters Supersonic flow Aerodynamic configurations |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910704031603321 |
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Rizk Yehia M.
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| Moffett Field, CA : , : National Aeronautics and Space Administration, Ames Research Center, , July 1985 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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USSAERO version D computer program development using ANSI standard FORTRAN 77 and DI-3000 graphics / / Michael R. Wiese
| USSAERO version D computer program development using ANSI standard FORTRAN 77 and DI-3000 graphics / / Michael R. Wiese |
| Autore | Wiese Michael R. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , May 1986 |
| Descrizione fisica | 1 online resource (viii, 97 pages) |
| Collana | NASA/CR |
| Soggetto topico |
Computer graphics
Aerodynamic characteristics Subsonic flow Pressure distribution Supersonic flow |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910709752703321 |
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Wiese Michael R.
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| Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , May 1986 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Validation of WIND for a series of inlet flows / / John W. Slater, John M. Abbott, and Richard H. Cavicchi
| Validation of WIND for a series of inlet flows / / John W. Slater, John M. Abbott, and Richard H. Cavicchi |
| Autore | Slater John W. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , October 2002 |
| Descrizione fisica | 1 online resource (13 pages) : illustrations (some color) |
| Collana | NASA/TM |
| Soggetto topico |
Computational fluid dynamics
Inlet flow Subsonic flow Supersonic flow Hypersonic flow |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910705661003321 |
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Slater John W.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , October 2002 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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VORCAM : a computer program for calculating vortex lift effect of cambered wings by the suction analogy / / C. Edward Lan and Jen-Fu Chang
| VORCAM : a computer program for calculating vortex lift effect of cambered wings by the suction analogy / / C. Edward Lan and Jen-Fu Chang |
| Autore | Lan C. Edward (Chuan-Tau Edward), <1935-> |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , November 1981 |
| Descrizione fisica | 1 online resource (122 pages) : illustrations |
| Collana | NASA/CR |
| Soggetto topico |
Computer programs
Cambered wings Supersonic flow User manuals (computer programs) Subsonic flow |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | VORCAM |
| Record Nr. | UNINA-9910709665303321 |
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Lan C. Edward (Chuan-Tau Edward), <1935->
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , November 1981 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Wind-tunnel and flight-test results for the measurements of flow variables at supersonic speeds using improved wedge and conical probes / / Percy J. Bobbitt [and four others]
| Wind-tunnel and flight-test results for the measurements of flow variables at supersonic speeds using improved wedge and conical probes / / Percy J. Bobbitt [and four others] |
| Autore | Bobbitt Percy J. |
| Pubbl/distr/stampa | Edwards, CA : , : National Aeronautics and Space Administration, Dryden Flight Research Center, , 2012 |
| Descrizione fisica | 1 online resource (58 pages) : illustrations (some color) |
| Collana | NASA/TM |
| Soggetto topico |
Supersonic flow
Wind tunnel tests Wedges Conical bodies Conical flow Cylindrical bodies Orifices Flight tests Flow distribution |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910704686003321 |
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Bobbitt Percy J.
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| Edwards, CA : , : National Aeronautics and Space Administration, Dryden Flight Research Center, , 2012 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Wind-US code contributions to the first AIAA Shock Boundary Layer Interaction Prediction Workshop / / Nicholas J. Georgiadis, Manan A. Vyas, and Dennis A. Yoder
| Wind-US code contributions to the first AIAA Shock Boundary Layer Interaction Prediction Workshop / / Nicholas J. Georgiadis, Manan A. Vyas, and Dennis A. Yoder |
| Autore | Georgiadis Nicholas J. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , 2013 |
| Descrizione fisica | 1 online resource (6 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Turbulent boundary layer
Computational fluid dynamics K-omega turbulence model Oblique shock waves Supersonic flow Computational grids |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910704910503321 |
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Georgiadis Nicholas J.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , 2013 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Soggetto topico
-
Supersonic flow
(29)
- Computational fluid dynamics (5)
- Subsonic flow (4)
- Wind tunnel tests (4)
- Mach number (3)