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Freestream Mach-number and temperature measurement in NASA Langley's 20-inch supersonic wind tunnel using laser-induced thermal acoustics / / Gregory C. Herring, R. Jeffrey Balla, and George B. Beeler



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Autore: Herring Gregory C. Visualizza persona
Titolo: Freestream Mach-number and temperature measurement in NASA Langley's 20-inch supersonic wind tunnel using laser-induced thermal acoustics / / Gregory C. Herring, R. Jeffrey Balla, and George B. Beeler Visualizza cluster
Pubblicazione: Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , September 2020
Descrizione fisica: 1 online resource (45 pages, 1 unnumbered page) : color illustrations
Soggetto topico: Mach number
Temperature
Freestream measurement
Laser-induced thermal acoustics (LITA)
20-inch supersonic wind tunnel (SWT)
Persona (resp. second.): BallaR. Jeffrey
BeelerGeorge B.
Note generali: "September 2020."
Altri titoli varianti: Freestream Mach-number and temperature measurement in National Aeronautics and Space Administration Langley's 20-inch supersonic wind tunnel using laser-induced thermal acoustics
Titolo autorizzato: Freestream Mach-number and temperature measurement in NASA Langley's 20-inch supersonic wind tunnel using laser-induced thermal acoustics  Visualizza cluster
Formato: Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione: Inglese
Record Nr.: 9910713933803321
Lo trovi qui: Univ. Federico II
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