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A comprehensive analysis of the X-15 flight 3-65 accident / / Cornelius J. Dennehy [and three others]
| A comprehensive analysis of the X-15 flight 3-65 accident / / Cornelius J. Dennehy [and three others] |
| Autore | Dennehy Cornelius J. |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , October 2014 |
| Descrizione fisica | 1 online resource (107 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Manned spacecraft
Aircraft accidents Flight control Hypersonic flight Failure modes Aerospace systems |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910703551303321 |
Dennehy Cornelius J.
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , October 2014 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Development and demonstration of a computational tool for the analysis of particle vitiation effects in hypersonic propulsion test facilities [[electronic resource] /] / Hugh Douglas Perkins
| Development and demonstration of a computational tool for the analysis of particle vitiation effects in hypersonic propulsion test facilities [[electronic resource] /] / Hugh Douglas Perkins |
| Autore | Perkins Hugh Douglas |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2010] |
| Descrizione fisica | 1 online resource (vii, 91 pages) : illustrations (color) |
| Collana | NASA/TM |
| Soggetto topico |
Hypersonic flight
Test facilities Air breathing engines Computational fluid dynamics Mathematical models Spacecraft propulsion Contamination Particle mass |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910700151203321 |
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Perkins Hugh Douglas
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2010] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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The effect of magnetohydrodynamic (MHD) energy bypass on specific thrust for a supersonic turbojet engine [[electronic resource] /] / Theresa L. Benyo ; prepared for the 48th Aerospace Sciences Meeting sponsored by the American Institute of Aeronautics and Astronautics, Orlando, Florida, January 4-7, 2010
| The effect of magnetohydrodynamic (MHD) energy bypass on specific thrust for a supersonic turbojet engine [[electronic resource] /] / Theresa L. Benyo ; prepared for the 48th Aerospace Sciences Meeting sponsored by the American Institute of Aeronautics and Astronautics, Orlando, Florida, January 4-7, 2010 |
| Autore | Benyo Theresa L |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2010] |
| Descrizione fisica | 1 online resource (13 pages) : illustrations (chiefly color) |
| Collana | NASA/TM |
| Soggetto topico |
Magnetohydrodynamics
Thermodynamic cycles Turbojet engines Thermal conductivity Supersonic speed Specific impulse Enthalpy Hypersonic flight |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Effect of magnetohydrodynamic |
| Record Nr. | UNINA-9910700383203321 |
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Benyo Theresa L
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2010] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Extraction of stability and control derivatives from orbiter flight data / / Kenneth W. Iliff and Mary F. Shafer
| Extraction of stability and control derivatives from orbiter flight data / / Kenneth W. Iliff and Mary F. Shafer |
| Autore | Iliff Kenneth W. |
| Pubbl/distr/stampa | [Washington, D.C.] : , : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, , June 1993 |
| Descrizione fisica | 1 online resource (46 pages) : illustrations |
| Collana | NASA technical memorandum |
| Soggetto topico |
Aerodynamic stability
Flight envelopes Hypersonic flight Space Shuttle orbiters Stability derivatives |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910705736603321 |
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Iliff Kenneth W.
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| [Washington, D.C.] : , : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, , June 1993 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Finite-element analysis of a Mach-8 flight test article using nonlinear contact elements / / W. Lance Richards
| Finite-element analysis of a Mach-8 flight test article using nonlinear contact elements / / W. Lance Richards |
| Autore | Richards W. Lance |
| Pubbl/distr/stampa | [Washington, D.C.] : , : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, , June 1997 |
| Descrizione fisica | 1 online resource (14 pages) : illustrations |
| Collana | NASA technical memorandum |
| Soggetto topico |
Finite element method
Hypersonic speed Structural design Hypersonic flight Nonlinearity |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910707027003321 |
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Richards W. Lance
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| [Washington, D.C.] : , : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, , June 1997 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Highlights from a Mach 4 experimental demonstration of inlet mode transition for Turbine-Based Combined Cycle hypersonic propulsion / / Lancert E. Foster [and three others]
| Highlights from a Mach 4 experimental demonstration of inlet mode transition for Turbine-Based Combined Cycle hypersonic propulsion / / Lancert E. Foster [and three others] |
| Autore | Foster Lancert E. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , 2012 |
| Descrizione fisica | 1 online resource (13 pages) : illustrations (some color) |
| Collana | NASA/TM |
| Soggetto topico |
Engine inlets
Hypersonic flight Supersonic speed Air breathing engines Supersonic combustion ramjet engines Specific impulse Propulsion system configurations |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910704671703321 |
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Foster Lancert E.
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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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The mothball, sustainment, and proposed reactivation of the hypersonic tunnel facility (HTF) at NASA Glenn Research Center Plum Brook Station / / Scott R. Thomas [and four others]
| The mothball, sustainment, and proposed reactivation of the hypersonic tunnel facility (HTF) at NASA Glenn Research Center Plum Brook Station / / Scott R. Thomas [and four others] |
| Autore | Thomas Scott R (Engineer) |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , December 2010 |
| Descrizione fisica | 1 online resource (14 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Hypersonic wind tunnels
Test facilities Hypersonic flight Hypersonic speed Propulsion |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Mothball, sustainment, and proposed reactivation of the hypersonic tunnel facility |
| Record Nr. | UNINA-9910700981503321 |
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Thomas Scott R (Engineer)
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , December 2010 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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NESC review of the 8-Foot High Temperature Tunnel (HTT) oxygen storage pressure vessel inspection requirements [[electronic resource] /] / Michael Gilbert ... [and others]
| NESC review of the 8-Foot High Temperature Tunnel (HTT) oxygen storage pressure vessel inspection requirements [[electronic resource] /] / Michael Gilbert ... [and others] |
| Pubbl/distr/stampa | Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2009] |
| Descrizione fisica | 1 online resource (29 pages) : illustrations |
| Altri autori (Persone) | GilbertMichael |
| Collana | NASA/TM- |
| Soggetto topico |
High temperature
Liquid oxygen Methane Propulsion system configurations Hypersonic flight Cryogenics Oxygen Pressure vessels Propulsion system performance |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | NESC review of the 8-Foot High Temperature Tunnel |
| Record Nr. | UNINA-9910697062803321 |
| Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2009] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Status of turbulence modeling for hypersonic propulsion flowpaths [[electronic resource] / Nicholas J. Geogiadis ... [and others]]
| Status of turbulence modeling for hypersonic propulsion flowpaths [[electronic resource] / Nicholas J. Geogiadis ... [and others]] |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012] |
| Descrizione fisica | 1 online resource (28 pages) : illustrations (some color) |
| Altri autori (Persone) | GeorgiadisNicholas J |
| Collana | NASA/TM |
| Soggetto topico |
Turbulent boundary layer
Hypersonic flight Large eddy simulation Supersonic combustion ramjet engines Reynolds averaging Shock waves Turbulence effects Turbulent flow Navier-Stokes equation |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910702012703321 |
| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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