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1-by 1- foot supersonic wind tunnel sidewall flowfield compression plate study / / Christopher J. Peters, Christine M. Pastor-Barsi, and David O. Davis
| 1-by 1- foot supersonic wind tunnel sidewall flowfield compression plate study / / Christopher J. Peters, Christine M. Pastor-Barsi, and David O. Davis |
| Autore | Peters Christopher J (Christopher John) |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , November 2020 |
| Descrizione fisica | 1 online resource (53 pages) : illustrations (chiefly color) |
| Collana | NASA/TM |
| Soggetto topico |
Fluid mechanics
Thermodynamics Wind tunnel tests Supersonic flow |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | One-by one- foot supersonic wind tunnel sidewall flowfield compression plate study |
| Record Nr. | UNINA-9910715241403321 |
Peters Christopher J (Christopher John)
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , November 2020 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Application of a Runge-Kutta scheme for high-speed inviscid internal flows [[electronic resource] /] / Anutosh Moitra, Eli Turkel, Ajay Kumar
| Application of a Runge-Kutta scheme for high-speed inviscid internal flows [[electronic resource] /] / Anutosh Moitra, Eli Turkel, Ajay Kumar |
| Autore | Moitra Anutosh |
| Pubbl/distr/stampa | Hampton, Va. : , : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, : Universities Space Research Association, , [1986] |
| Descrizione fisica | 1 online resource (i, 24 pages) : illustrations |
| Altri autori (Persone) |
TurkelE
KumarAjay |
| Collana |
NASA contractor report
ICASE report |
| Soggetto topico |
Computational fluid dynamics
Inviscid flow Runge-Kutta method Supersonic flow |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910701830703321 |
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Moitra Anutosh
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| Hampton, Va. : , : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, : Universities Space Research Association, , [1986] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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An asymptotic analysis of supersonic reacting mixing layers [[electronic resource] /] / T. L. Jackson, M. Y. Hussaini
| An asymptotic analysis of supersonic reacting mixing layers [[electronic resource] /] / T. L. Jackson, M. Y. Hussaini |
| Autore | Jackson T. L |
| Pubbl/distr/stampa | Hampton, Va. : , : Universities Space Research Association, Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, , [1987] |
| Descrizione fisica | 1 online resource (17 pages) |
| Altri autori (Persone) | HussainiM. Yousuff |
| Collana |
NASA contractor report
ICASE report |
| Soggetto topico |
Asymptotic methods
Chemical reactions Laminar mixing Mixing layers (fluids) Supersonic flow |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910701932703321 |
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Jackson T. L
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| Hampton, Va. : , : Universities Space Research Association, Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, , [1987] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Comparison of various supersonic turbine tip designs to minimize aerodynamic loss and tip heating [[electronic resource] /] / Vikram Shyam, Ali Ameri
| Comparison of various supersonic turbine tip designs to minimize aerodynamic loss and tip heating [[electronic resource] /] / Vikram Shyam, Ali Ameri |
| Autore | Shyam Vikram |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012] |
| Descrizione fisica | 1 online resource (8 pages) : illustrations (some color) |
| Altri autori (Persone) | AmeriAli |
| Collana | NASA/TM |
| Soggetto topico |
Computational fluid dynamics
Supersonic turbines Blade tips Supersonic flow Rotor aerodynamics Axial flow turbines Supersonic heat transfer Contours |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910702216503321 |
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Shyam Vikram
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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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Computational analysis of a low-boom supersonic inlet [[electronic resource] /] / Rodrick V. Chima
| Computational analysis of a low-boom supersonic inlet [[electronic resource] /] / Rodrick V. Chima |
| Autore | Chima Rodrick V |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2011] |
| Descrizione fisica | 1 online resource (14 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Computational fluid dynamics
Engine inlets Supersonic aircraft Supersonic inlets Inlet airframe configurations Overpressure Supersonic flow Sonic booms Wind tunnel tests |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910701537703321 |
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Chima Rodrick V
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2011] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Entropy stable wall boundary conditions for the compressible Navier-Stokes equations / / Matteo Parsani, Mark H. Carpenter, and Eric J. Nielsen
| Entropy stable wall boundary conditions for the compressible Navier-Stokes equations / / Matteo Parsani, Mark H. Carpenter, and Eric J. Nielsen |
| Autore | Parsani Matteo |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , June 2014 |
| Descrizione fisica | 1 online resource (47 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Navier-Stokes equation
Galerkin method Supersonic flow Three dimensional flow Finite element method Finite volume method Finite difference theory |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910702739303321 |
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Parsani Matteo
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , June 2014 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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An estimate of the supersonic flow field about an axisymmetric body with an N wave pressure trace / / by Roger W. Luidens
| An estimate of the supersonic flow field about an axisymmetric body with an N wave pressure trace / / by Roger W. Luidens |
| Autore | Luidens Roger W. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, , December 1968 |
| Descrizione fisica | 1 online resource (ii, 25 pages) : illustrations |
| Collana | NASA/TN |
| Soggetto topico |
Sonic booms
Supersonic flow Sonic boom |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910716031303321 |
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Luidens Roger W.
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| Washington, D.C. : , : National Aeronautics and Space Administration, , December 1968 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Experimental and theoretical study of longitudinal aerodynamic characteristics of delta and double-delta wings at Mach numbers of 1.60, 1.90, and 2.16 / / Richard M. Wood and Peter F. Covell
| Experimental and theoretical study of longitudinal aerodynamic characteristics of delta and double-delta wings at Mach numbers of 1.60, 1.90, and 2.16 / / Richard M. Wood and Peter F. Covell |
| Autore | Wood Richard M. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , July 1985 |
| Descrizione fisica | 1 online resource (119 pages) : illustrations |
| Collana | NASA/TP |
| Soggetto topico |
Supersonic airfoils
Delta wings Supersonic flow Aerodynamic drag Mach number Airplanes - Wings, Triangular - Aerodynamics |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910709794403321 |
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Wood Richard M.
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| Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , July 1985 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Experimental and theoretical study of the longitudinal aerodynamic characteristics of delta and double-delta wings at mach numbers of 1.60, 1.90, and 2.16 / / Richard M. Wood and Peter F. Covell
| Experimental and theoretical study of the longitudinal aerodynamic characteristics of delta and double-delta wings at mach numbers of 1.60, 1.90, and 2.16 / / Richard M. Wood and Peter F. Covell |
| Autore | Wood Richard M. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , July 1985 |
| Descrizione fisica | 1 online resource (119 pages, 1 unnumbered page) : illustrations |
| Collana | NASA/TP |
| Soggetto topico |
Delta wings
Supersonic airfoils Mach number Sweptback wings Supersonic flow |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910709981303321 |
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Wood Richard M.
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| Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , July 1985 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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An experimental study of turbulent skin friction reduction in supersonic flow using a microblowing technique / / Danny P. Hwang
| An experimental study of turbulent skin friction reduction in supersonic flow using a microblowing technique / / Danny P. Hwang |
| Autore | Hwang Danny P. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , December 1999 |
| Descrizione fisica | 1 online resource (7 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Skin friction
Friction reduction Turbulent flow Supersonic flow Porous plates |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910706132103321 |
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Hwang Danny P.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , December 1999 | ||
| 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)