Info
- Utilizzare la checkbox di selezione a fianco di ciascun documento per attivare le funzionalità di stampa, invio email, download nei formati disponibili del (i) record.
Conical shock-strength determination on low-sonic-boom aircraft model by doppler global velocimetry [[electronic resource] /] / Gregory C. Herring and James F. Meyers
| Conical shock-strength determination on low-sonic-boom aircraft model by doppler global velocimetry [[electronic resource] /] / Gregory C. Herring and James F. Meyers |
| Autore | Herring Gregory C |
| Pubbl/distr/stampa | Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2011] |
| Descrizione fisica | 1 online resource (29 pages) : illustrations (some color) |
| Altri autori (Persone) | MeyersJames F |
| Collana | NASA/TM |
| Soggetto topico |
Velocity measurement
Sonic booms Flow characteristics Supersonic speed Oblique shock waves |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Conical shock strength determination on low sonic boom aircraft model by doppler global velocimetry |
| Record Nr. | UNINA-9910700812003321 |
Herring Gregory C
|
||
| Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2011] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
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 |
|
Hirt Stefanie M
|
||
| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2009] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Micro-ramp flow control for oblique shock interactions [[electronic resource] ] : comparisons of computational and experimental data / / Stefanie M. Hirt, David B. Reich, Michael B. O'Connor
| Micro-ramp flow control for oblique shock interactions [[electronic resource] ] : comparisons of computational and experimental data / / Stefanie M. Hirt, David B. Reich, Michael B. O'Connor |
| Autore | Hirt Stefanie M |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012] |
| Descrizione fisica | 1 online resource (14 pages) : illustrations (some color) |
| Altri autori (Persone) |
ReichDavid B
O'ConnorMichael B |
| Collana | NASA/TM |
| Soggetto topico |
Vortex generators
Computational fluid dynamics Oblique shock waves Flow distribution |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Micro-ramp flow control for oblique shock interactions |
| Record Nr. | UNINA-9910702236603321 |
|
Hirt Stefanie M
|
||
| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Shock generation and control using DBD plasma actuators : SBIR phase I final report / / by Mehul P. Patel [and four others]
| Shock generation and control using DBD plasma actuators : SBIR phase I final report / / by Mehul P. Patel [and four others] |
| Autore | Patel Mehul P. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012] |
| Descrizione fisica | 1 online resource (34 pages) : color illustrations |
| Collana | [NASA contractor report] |
| Soggetto topico |
Actuators
Dielectrics Shock tests Wind tunnel tests Aircraft engines Turbulent boundary layer Boundary layer separation Supersonic inlets Oblique shock waves |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Shock generation and control using DBD plasma actuators |
| Record Nr. | UNINA-9910702110403321 |
|
Patel Mehul P.
|
||
| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Wind-US code contributions to the first AIAA Shock Boundary Layer Interaction Prediction Workshop / / Nicholas J. Georgiadis, Manan A. Vyas, and Dennis A. Yoder
| Wind-US code contributions to the first AIAA Shock Boundary Layer Interaction Prediction Workshop / / Nicholas J. Georgiadis, Manan A. Vyas, and Dennis A. Yoder |
| Autore | Georgiadis Nicholas J. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , 2013 |
| Descrizione fisica | 1 online resource (6 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Turbulent boundary layer
Computational fluid dynamics K-omega turbulence model Oblique shock waves Supersonic flow Computational grids |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910704910503321 |
|
Georgiadis Nicholas J.
|
||
| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , 2013 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
