|
|
|
|
|
|
|
|
|
1. |
Record Nr. |
UNINA9910706214703321 |
|
|
Autore |
VanFossen G. James |
|
|
Titolo |
Augmentation of stagnation region heat transfer due to turbulence from a DLN can combustor / / G. James Van Fossen, Ronald S. Bunker |
|
|
|
|
|
|
|
Pubbl/distr/stampa |
|
|
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , July 2000 |
|
|
|
|
|
|
|
|
|
Descrizione fisica |
|
1 online resource (9 pages) : illustrations |
|
|
|
|
|
|
Collana |
|
|
|
|
|
|
Soggetti |
|
Augmentation |
Stagnation point |
Flow distribution |
Heat transfer |
Gas turbines |
Turbulent flow |
Isotropic turbulence |
|
|
|
|
|
|
|
|
Lingua di pubblicazione |
|
|
|
|
|
|
Formato |
Materiale a stampa |
|
|
|
|
|
Livello bibliografico |
Monografia |
|
|
|
|
|
Note generali |
|
"July 2000." |
"Prepared for the 45th International Gas Turbine and Aeroengine Technical Congress sponsored by the American Society of Mechanical Engineers, Munich, Germany, May 8-11, 2000." |
"Performing organization: National Aeronautics and Space Administration, John H. Glenn Research Center at Lewis Field"--Report documentation page. |
"ASME 2000-GT-0215." |
|
|
|
|
|
|
|
|
Nota di bibliografia |
|
Includes bibliographical references (pages 8-9). |
|
|
|
|
|
| |