Vai al contenuto principale della pagina
Autore: |
Castner Raymond S
![]() |
Titolo: |
Wind tunnel model design for the study of plume effects on sonic boom for isolated exhaust nozzles [[electronic resource] /] / Raymond S. Castner ; prepared for the 45th Joint Propulsion Conference and Exhibit cosponsored by AIAA, ASME, SAE, and ASEE, Denver, Colorado, August 2-5, 2009
![]() |
Pubblicazione: | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2010] |
Descrizione fisica: | 1 online resource (10 pages) : illustrations |
Soggetto topico: | Wind tunnel tests |
Supersonic aircraft | |
Aerodynamic configurations | |
Low cost | |
Supersonic wind tunnels | |
Wind tunnel models | |
Sonic booms | |
Static pressure | |
Pressure sensors | |
Exhaust nozzles | |
Note generali: | Title from title screen (viewed on Oct. 7, 2010). |
"April 2010." | |
"AIAA-2009-5369." | |
Nota di bibliografia: | Includes bibliographical references (page 10) |
Titolo autorizzato: | Wind tunnel model design for the study of plume effects on sonic boom for isolated exhaust nozzles ![]() |
Formato: | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione: | Inglese |
Record Nr.: | 9910699547103321 |
Lo trovi qui: | Univ. Federico II |
Opac: | Controlla la disponibilità qui |