01968nam 2200469I 450 991071393380332120201211082618.0(CKB)5470000002506326(OCoLC)1200761100(EXLCZ)99547000000250632620201019j202009 ua 0engur|||||||||||txtrdacontentcrdamediacrrdacarrierFreestream 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. BeelerHampton, Virginia :National Aeronautics and Space Administration, Langley Research Center,September 2020.1 online resource (45 pages, 1 unnumbered page) color illustrationsNASA/TM ;2020-5007323"September 2020."Freestream Mach-number and temperature measurement in National Aeronautics and Space Administration Langley's 20-inch supersonic wind tunnel using laser-induced thermal acousticsMach numbernasatTemperaturenasatFreestream measurementnasatLaser-induced thermal acoustics (LITA)nasat20-inch supersonic wind tunnel (SWT)nasatMach number.Temperature.Freestream measurement.Laser-induced thermal acoustics (LITA)20-inch supersonic wind tunnel (SWT)Herring Gregory C.1394410Balla R. JeffreyBeeler George B.Langley Research Center,GPOGPOBOOK9910713933803321Freestream Mach-number and temperature measurement in NASA Langley's 20-inch supersonic wind tunnel using laser-induced thermal acoustics3468833UNINA