Info
Numerical simulations of a Quiet SuperSonic Technology (QueSST) aircraft preliminary design / / David J. Friedlander, Christopher M. Heath, and Raymond S. Castner
| Numerical simulations of a Quiet SuperSonic Technology (QueSST) aircraft preliminary design / / David J. Friedlander, Christopher M. Heath, and Raymond S. Castner |
| Autore | Friedlander David J. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , October 2018 |
| Descrizione fisica | 1 online resource (55 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Computational fluid dynamics
Supersonic aircraft Reynolds averaging Grid refinement (mathematics) Computerized simulation |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Numerical simulations of a Quiet SuperSonic Technology |
| Record Nr. | UNINA-9910711552903321 |
Friedlander David J.
|
||
| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , October 2018 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Reynolds-averaged Navier-Stokes solutions to flat plate film cooling scenarios [[electronic resource] /] / Perry L. Johnson, Vikram Shyam and Chunill Hah
| Reynolds-averaged Navier-Stokes solutions to flat plate film cooling scenarios [[electronic resource] /] / Perry L. Johnson, Vikram Shyam and Chunill Hah |
| Autore | Johnson Perry L |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2011] |
| Descrizione fisica | 1 online resource (21 pages) : color illustrations |
| Altri autori (Persone) |
ShyamVikram
HahC |
| Collana | NASA/TM |
| Soggetto topico |
Film cooling
Flat plates Navier-Stokes equation Reynolds averaging Mathematical models Grid refinement (mathematics) Gas turbine engines |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910701152503321 |
|
Johnson Perry L
|
||
| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2011] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Updates to simulation of a single-element lean-direct injection combustor using a polyhedral mesh derived from hanging-node elements / / Changju Thomas Wey and Nan-Suey Liu
| Updates to simulation of a single-element lean-direct injection combustor using a polyhedral mesh derived from hanging-node elements / / Changju Thomas Wey and Nan-Suey Liu |
| Autore | Wey Changju Thomas |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , March 2014 |
| Descrizione fisica | 1 online resource (14 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Computational fluid dynamics
Navier-Stokes equation Grid generation (mathematics) Large eddy simulation Grid refinement (mathematics) |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910703640203321 |
|
Wey Changju Thomas
|
||
| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , March 2014 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
