| |
|
|
|
|
|
|
|
|
1. |
Record Nr. |
UNINA9910701912103321 |
|
|
Autore |
Castner Raymond S |
|
|
Titolo |
Exhaust nozzle plume effects on sonic boom test results for isolated nozzles [[electronic resource] /] / Raymond S. Castner ; prepared for the 28th Applied Aerodynamics Conference sponsored by the American Institute of Aeronautics and Astronautics, Chicago, Illinois, June 28-July 1, 20 |
|
|
|
|
|
|
|
Pubbl/distr/stampa |
|
|
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2011] |
|
|
|
|
|
|
|
|
|
Descrizione fisica |
|
1 online resource (16 pages) : color illustrations |
|
|
|
|
|
|
Collana |
|
|
|
|
|
|
Soggetti |
|
Exhaust nozzles |
Nozzle flow |
Plumes |
Supersonic aircraft |
Computational fluid dynamics |
Nozzle geometry |
Pressure ratio |
Shock waves |
Elastic waves |
|
|
|
|
|
|
|
|
Lingua di pubblicazione |
|
|
|
|
|
|
Formato |
Materiale a stampa |
|
|
|
|
|
Livello bibliografico |
Monografia |
|
|
|
|
|
Note generali |
|
Title from title screen (viewed on Aug. 30, 2012). |
"December 2011." |
"AIAA-2010-4936." |
|
|
|
|
|
|
|
|
Nota di bibliografia |
|
Includes bibliographical references (page 16). |
|
|
|
|
|
| |