|
|
|
|
|
|
|
|
|
1. |
Record Nr. |
UNINA9910706576003321 |
|
|
Autore |
Steffen Christopher J. |
|
|
Titolo |
Computational analysis of the combustion process in an axisymmetric,RBCC flowpath / / Christopher J. Steffen, Shaye Yungster |
|
|
|
|
|
|
|
Pubbl/distr/stampa |
|
|
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , February 2001 |
|
|
|
|
|
|
|
|
|
Descrizione fisica |
|
1 online resource (15 pages) : illustrations |
|
|
|
|
|
|
Collana |
|
|
|
|
|
|
Soggetti |
|
Computational fluid dynamics |
Numerical analysis |
Combustion physics |
Three dimensional models |
Supersonic combustion ramjet engines |
Simulation |
|
|
|
|
|
|
|
|
Lingua di pubblicazione |
|
|
|
|
|
|
Formato |
Materiale a stampa |
|
|
|
|
|
Livello bibliografico |
Monografia |
|
|
|
|
|
Note generali |
|
"February 2001." |
"Prepared for the 37th Combustion Subcommittee, 25th Airbreathing Propulsion Subcommittee, and 19th Propulsion Systems Hazards Subcommittee Joint Meeting cosponsored by the Joint Army-Navy-Air Force Interagency Propulsion Committee, Monterey, California, November 13-17, 2000." |
"Performing organization: National Aeronautics and Space Administration, John H. Glenn Research Center at Lewis Field"--Report documentation page. |
|
|
|
|
|
|
|
|
Nota di bibliografia |
|
Includes bibliographical references (page 15). |
|
|
|
|
|
| |