Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control / / Scott C. Asbury and Craig A. Hunter
Pubbl/distr/stampa
Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , August 1999
Descrizione fisica
1 online resource (134 pages) : illustrations
Collana
NASA/TM ; ; 1999-209513
Soggetti
Exhaust nozzles
Porosity
Hole geometry (mechanics)
Cavities
Thrust vector control
Lingua di pubblicazione
Inglese
Formato
Materiale a stampa
Livello bibliografico
Monografia
Note generali
"August 1999."
"Performing organization: NASA Langley Research Center"--Report documentation page.
Nota di bibliografia
Includes bibliographical references (pages 19-20).