Analysis of buzz in a supersonic inlet [[electronic resource] /] / Rodrick V. Chima
| Analysis of buzz in a supersonic inlet [[electronic resource] /] / Rodrick V. Chima |
| Autore | Chima Rodrick V |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012] |
| Descrizione fisica | 1 online resource (36 pages) : illustrations (some color) |
| Collana | NASA/TM |
| Soggetto topico |
Computational fluid dynamics
Supersonic wind tunnels Acoustic resonance Frequency response High frequencies Mach number Inlet pressure Supersonic speed |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910702114103321 |
Chima Rodrick V
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012] | ||
| Lo trovi qui: Univ. Federico II | ||
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Axisymmetric calculations of a low-boom inlet in a supersonic wind tunnel [[electronic resource] /] / Rodrick V. Chima and Stefanie M. Hirt, Robert Reger
| Axisymmetric calculations of a low-boom inlet in a supersonic wind tunnel [[electronic resource] /] / Rodrick V. Chima and Stefanie M. Hirt, Robert Reger |
| Autore | Chima Rodrick V |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2011] |
| Descrizione fisica | 1 online resource (12 pages) : illustrations (chiefly color) |
| Altri autori (Persone) |
HirtStefanie M
RegerRobert |
| Collana | NASA/TM |
| Soggetto topico |
Supersonic inlets
Computational fluid dynamics Mass flow Flight paths Supersonic aircraft Stability |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910701560503321 |
Chima Rodrick V
|
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2011] | ||
| 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 |
Chima Rodrick V
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||
| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2011] | ||
| Lo trovi qui: Univ. Federico II | ||
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A three-dimensional unsteady CFD model of compressor stability [[electronic resource] /] / Rodrick V. Chima ; prepared for Turbo Expo 2006 sponsored by the American Society of Mechanical Engineers, Barcelona, Spain, May 8-11, 2006
| A three-dimensional unsteady CFD model of compressor stability [[electronic resource] /] / Rodrick V. Chima ; prepared for Turbo Expo 2006 sponsored by the American Society of Mechanical Engineers, Barcelona, Spain, May 8-11, 2006 |
| Autore | Chima Rodrick V |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2006] |
| Descrizione fisica | 1 online resource (12 pages) : illustrations |
| Collana | NASA/TM- |
| Soggetto topico |
Computational fluid dynamics
Navier-Stokes equation Turbocompressors Flow stability Unsteady flow Rotor aerodynamics |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910697162903321 |
Chima Rodrick V
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2006] | ||
| Lo trovi qui: Univ. Federico II | ||
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