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Assessment of computational fluid dynamics (CFD) models for shock boundary-layer interaction [[electronic resource] /] / James R. DeBonis ... [and others] ; prepared for the 28th Applied Aerodynamics Conference sponsored by the American Institute of Aeronautics and Astronautics, Chicago, Illinois, June 28 to July 1, 2010
| Assessment of computational fluid dynamics (CFD) models for shock boundary-layer interaction [[electronic resource] /] / James R. DeBonis ... [and others] ; prepared for the 28th Applied Aerodynamics Conference sponsored by the American Institute of Aeronautics and Astronautics, Chicago, Illinois, June 28 to July 1, 2010 |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2011] |
| Descrizione fisica | 1 online resource (28 pages) : color illustrations |
| Altri autori (Persone) | DeBonisJames R |
| Collana | NASA/TM |
| Soggetto topico |
Shock wave interaction
Boundary layers Turbulence models Computational fluid dynamics Navier-Stokes equation Large eddy simulation |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Assessment of computational fluid dynamics |
| Record Nr. | UNINA-9910700980003321 |
| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2011] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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CFD validation experiment of a Mach 2.5 axisymmetric shock-wave/boundary-layer interaction / / David O. Davis
| CFD validation experiment of a Mach 2.5 axisymmetric shock-wave/boundary-layer interaction / / David O. Davis |
| Autore | Davis David O. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , September 2015 |
| Descrizione fisica | 1 online resource (13 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Boundary layers
Computational fluid dynamics Shock wave interaction Flow measurement Turbulent flow |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Computational fluid dynamics validation experiment of a Mach 2.5 axisymmetric shock wave boundary layer interaction |
| Record Nr. | UNINA-9910704277603321 |
Davis David O.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , September 2015 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Entry, descent, and landing with propulsive deceleration : supersonic retropropulsion wind tunnel testing / / Bryan Palaszewski
| Entry, descent, and landing with propulsive deceleration : supersonic retropropulsion wind tunnel testing / / Bryan Palaszewski |
| Autore | Palaszewski Bryan Alan Richard |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012] |
| Descrizione fisica | 1 online resource (25 pages) : illustrations |
| Collana | NASA/TM 2012-217746 |
| Soggetto topico |
Computational fluid dynamics
Planetary landing Aerodynamic brakes Landing aids Soft landing Landing sites Rocket engines Shock wave interaction Supersonic flight |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Entry, descent, and landing with propulsive deceleration |
| Record Nr. | UNINA-9910704623303321 |
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Palaszewski Bryan Alan Richard
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Estimation of supersonic stage separation aerodynamics of winged-body launch vehicles using response surface methods [[electronic resource] /] / Gary E. Erickson
| Estimation of supersonic stage separation aerodynamics of winged-body launch vehicles using response surface methods [[electronic resource] /] / Gary E. Erickson |
| Autore | Erickson Gary E |
| Pubbl/distr/stampa | Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2010] |
| Descrizione fisica | 1 online resource (v, 36 pages) : illustrations |
| Collana | NASA/TM- |
| Soggetto topico |
Aerodynamic characteristics
Control surfaces Launch vehicles Shock wave interaction Supersonic speed |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910697041703321 |
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Erickson Gary E
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| Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2010] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Exhaust nozzle plume and shock wave interaction / / Raymond S. Castner, Alaa Elmiligui, Susan Cliff
| Exhaust nozzle plume and shock wave interaction / / Raymond S. Castner, Alaa Elmiligui, Susan Cliff |
| Autore | Castner Raymond S. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , 2013 |
| Descrizione fisica | 1 online resource (21 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Computational fluid dynamics
Shock wave interaction Convergent-divergent nozzles Sonic booms |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910704910603321 |
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Castner Raymond S.
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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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Experimental investigation of the application of microramp flow control to an oblique shock interaction [[electronic resource] /] / Stefanie M. Hirt and Bernhard H. Anderson ; prepared for the 47th Aerospace Sciences Meeting sponsored by the American Institute of Aeronautics and Astronautics, Orlando, Florida, January 5-8, 2009
| Experimental investigation of the application of microramp flow control to an oblique shock interaction [[electronic resource] /] / Stefanie M. Hirt and Bernhard H. Anderson ; prepared for the 47th Aerospace Sciences Meeting sponsored by the American Institute of Aeronautics and Astronautics, Orlando, Florida, January 5-8, 2009 |
| Autore | Hirt Stefanie M |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2009] |
| Descrizione fisica | 1 online resource (27 pages) : illustrations |
| Altri autori (Persone) | AndersonBernhard H |
| Collana | NASA TM- |
| Soggetto topico |
Oblique shock waves
Boundary layers Shock wave interaction Experiment design Factorial design |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910696924503321 |
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Hirt Stefanie M
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2009] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Numerical simulation of low-density shock-wave interactions / / Christopher E. Glass
| Numerical simulation of low-density shock-wave interactions / / Christopher E. Glass |
| Autore | Glass Christopher E (Christopher Earl), <1955-> |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , July 1999 |
| Descrizione fisica | 1 online resource (17 pages) : illustrations |
| Collana | NASA TM- |
| Soggetto topico |
Computational fluid dynamics
Computerized simulation Low density flow Shock wave interaction |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910706168703321 |
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Glass Christopher E (Christopher Earl), <1955->
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , July 1999 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Understanding the flow physics of shock boundary-layer interactions using CFD and numerical analyses / / David J. Friedlander
| Understanding the flow physics of shock boundary-layer interactions using CFD and numerical analyses / / David J. Friedlander |
| Autore | Friedlander David J. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , October 2013 |
| Descrizione fisica | 1 online resource (xvi, 105 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Computational fluid dynamics
Shock wave interaction Boundary layers Flow distribution Particle image velocimetry Large eddy simulation |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Understanding the flow physics of shock boundary layer interactions using Computational Fluid Dynamics and numerical analyses |
| Record Nr. | UNINA-9910702430903321 |
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Friedlander David J.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , October 2013 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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