Impingement of boundary-reflected disturbances originating at the nose of a body of revolution in the Langley Research Center 16-foot transonic tunnel / / Richard J. Re and Francis J. Capone
Pubbl/distr/stampa
Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , October 1998
Descrizione fisica
1 online resource (37 pages) : illustrations
Collana
NASA/TM ; ; 1998-208723
Soggetti
Supersonic transports
Supersonic speed
Static pressure
Shock waves
Mach number
Bow waves
Bodies of revolution
Lingua di pubblicazione
Inglese
Formato
Materiale a stampa
Livello bibliografico
Monografia
Note generali
"October 1998."
"Performing organization: NASA Langley Research Center"--Report documentation page.