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An approximate axisymmetric viscous shock layer aeroheating method for three-dimensional bodies / / Irina G. Brykina, Carl D. Scott
| An approximate axisymmetric viscous shock layer aeroheating method for three-dimensional bodies / / Irina G. Brykina, Carl D. Scott |
| Autore | Brykina Irina G. |
| Pubbl/distr/stampa | Houston, Texas : , : National Aeronautics and Space Administration, Lyndon B. Johnson Space Center, , May 1998 |
| Descrizione fisica | 1 online resource (iv, 28 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Flow measurement
Axisymmetric flow Aerodynamic heating Parabolic bodies Hypersonics Axisymmetric bodies Blunt bodies |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910705868703321 |
Brykina Irina G.
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| Houston, Texas : , : National Aeronautics and Space Administration, Lyndon B. Johnson Space Center, , May 1998 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Comparison of analysis with test for static loading of two hypersonic inflatable aerodynamic decelerator concepts / / Karen H. Lyle
| Comparison of analysis with test for static loading of two hypersonic inflatable aerodynamic decelerator concepts / / Karen H. Lyle |
| Autore | Lyle Karen H. |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , July 2015 |
| Descrizione fisica | 1 online resource (14 pages) : color illustration |
| Collana | NASA/TM |
| Soggetto topico |
Inflatable structures
Aerodynamic brakes Hypersonics Aerospace vehicles Reentry vehicles |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910704022403321 |
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Lyle Karen H.
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , July 2015 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Computational fluid dynamics (CFD) simulation of hypersonic turbine-based combined-cycle (TBCC) inlet mode transition [[electronic resource] /] / John W. Slater and John D. Saunders ; prepared for the 16th International Space Planes and Hypersonic Systems and Technologies Conference cosponsored by the AIAA, DLR, and DGLR, Bremen, Germany, October 19-22, 2009
| Computational fluid dynamics (CFD) simulation of hypersonic turbine-based combined-cycle (TBCC) inlet mode transition [[electronic resource] /] / John W. Slater and John D. Saunders ; prepared for the 16th International Space Planes and Hypersonic Systems and Technologies Conference cosponsored by the AIAA, DLR, and DGLR, Bremen, Germany, October 19-22, 2009 |
| Autore | Slater John W |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2010] |
| Descrizione fisica | 1 online resource (27 pages) : illustrations |
| Altri autori (Persone) | SaundersJohn D |
| Collana | NASA/TM |
| Soggetto topico |
Computational fluid dynamics 241
Data simulation Hypersonics Static pressure Supersonic combustion ramjet engines Wind tunnel tests Aerodynamics Boundary layers |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Computational fluid dynamics |
| Record Nr. | UNINA-9910699653003321 |
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Slater John W
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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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Control activity in support of NASA Turbine Based Combined Cycle (TBCC) research [[electronic resource] /] / Thomas J. Stueber ... [and others]
| Control activity in support of NASA Turbine Based Combined Cycle (TBCC) research [[electronic resource] /] / Thomas J. Stueber ... [and others] |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2010] |
| Descrizione fisica | 1 online resource (18 pages) : illustrations (some color) |
| Altri autori (Persone) | StueberThomas J |
| Collana | NASA/TM |
| Soggetto topico |
Hypersonics
Computerized simulation Aerodynamics Control systems design Propulsion Guidance (motion) Turbine engines Air breathing engines |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Control activity in support of NASA Turbine Based Combined Cycle |
| Record Nr. | UNINA-9910699506703321 |
| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2010] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Current capabilities and future directions in computational fluid dynamics [[electronic resource] /] / Committee to Assess Current Capabilities and Future Directions in Computational Fluid Dynamics, Aeronautics and Space Engineering Board, Commission on Engineering and Technical Systems, National Research Council
| Current capabilities and future directions in computational fluid dynamics [[electronic resource] /] / Committee to Assess Current Capabilities and Future Directions in Computational Fluid Dynamics, Aeronautics and Space Engineering Board, Commission on Engineering and Technical Systems, National Research Council |
| Pubbl/distr/stampa | Washington, D.C. : , : National Academy Press : , : Available from Aeronautics and Space Engineering Board, National Research Council, , 1986 |
| Descrizione fisica | 1 volume |
| Altri autori (Persone) | BradleyRichard G |
| Collana | NASA-CR |
| Soggetto topico |
Computational fluid dynamics
Computerized simulation Hypersonics Propulsion Steady flow Turbulent flow |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910698972203321 |
| Washington, D.C. : , : National Academy Press : , : Available from Aeronautics and Space Engineering Board, National Research Council, , 1986 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Effect of protuberance shape and orientation on Space Shuttle Orbiter boundary-layer transition [[electronic resource] /] / Rudolph A. King, Scott A. Berry, Michael A. Kegerise
| Effect of protuberance shape and orientation on Space Shuttle Orbiter boundary-layer transition [[electronic resource] /] / Rudolph A. King, Scott A. Berry, Michael A. Kegerise |
| Autore | King Rudolph A |
| Pubbl/distr/stampa | Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2008] |
| Descrizione fisica | 1 online resource (20 pages) : illustrations |
| Altri autori (Persone) |
BerryScott A
KegeriseMichael A |
| Collana | NASA TM- |
| Soggetto topico |
Boundary layer transition
Hypersonics Protuberances Space Shuttle orbiters Thermography Shapes Heat transfer |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910699550403321 |
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King Rudolph A
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| Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2008] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Hypersonic inflatable aerodynamic decelerator (HIAD) torus mechanical testing / / Tony Chen, Matthew R. Moholt, and Larry D. Hudson
| Hypersonic inflatable aerodynamic decelerator (HIAD) torus mechanical testing / / Tony Chen, Matthew R. Moholt, and Larry D. Hudson |
| Autore | Chen Tony |
| Pubbl/distr/stampa | Edwards, California : , : National Aeronautics and Space Administration, Armstrong Flight Research Center, , November 2017 |
| Descrizione fisica | 1 online resource (x, 60 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Hypersonics
Toruses Aerodynamic brakes Load tests Inflatable structures |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Hypersonic inflatable aerodynamic decelerator |
| Record Nr. | UNINA-9910706507803321 |
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Chen Tony
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| Edwards, California : , : National Aeronautics and Space Administration, Armstrong Flight Research Center, , November 2017 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Multidisciplinary analysis of a hypersonic engine / / M.E.M. Stewart [and four others]
| Multidisciplinary analysis of a hypersonic engine / / M.E.M. Stewart [and four others] |
| Autore | Stewart Mark E. M. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , October 2002 |
| Descrizione fisica | 1 online resource (11 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Hypersonics
Fluid dynamics Structural analysis Thermodynamics Supersonic combustion ramjet engines |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910705647003321 |
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Stewart Mark E. M.
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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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Operational experience in the Langley Expansion Tube with various testy gases / / Charles G. Miller
| Operational experience in the Langley Expansion Tube with various testy gases / / Charles G. Miller |
| Autore | Miller Charles G (Charles George), <1940-> |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, , Langley Research Center, , December 1977 |
| Descrizione fisica | 1 online resource (approximately 36 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Real gases
Hypersonics Hypervelocity |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910717190103321 |
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Miller Charles G (Charles George), <1940->
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| Hampton, Virginia : , : National Aeronautics and Space Administration, , Langley Research Center, , December 1977 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Preliminary structural sensitivity study of hypersonic inflatable aerodynamic decelerator using probabilistic methods / / Karen H. Lyle
| Preliminary structural sensitivity study of hypersonic inflatable aerodynamic decelerator using probabilistic methods / / Karen H. Lyle |
| Autore | Lyle Karen H. |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , July 2014 |
| Descrizione fisica | 1 online resource (14 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Large space structures
Hypersonics Aerodynamic loads Spacecraft design Structural analysis Mathematical models |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910702739103321 |
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Lyle Karen H.
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , July 2014 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Soggetto topico
-
Hypersonics
(11)
- Aerodynamic brakes (2)
- Aerodynamics (2)
- Computerized simulation (2)
- Inflatable structures (2)