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001 9910713933803321
005 20201211082618.0
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035   $a(EXLCZ)995470000002506326
100   $a20201019j202009    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aFreestream Mach-number and temperature measurement in NASA Langley's 20-inch supersonic wind tunnel using laser-induced thermal acoustics /$fGregory C. Herring, R. Jeffrey Balla, and George B. Beeler
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dSeptember 2020.
215   $a1 online resource (45 pages, 1 unnumbered page) $ccolor illustrations
225 1 $aNASA/TM ;$v2020-5007323
300   $a"September 2020."
517 3 $aFreestream Mach-number and temperature measurement in National Aeronautics and Space Administration Langley's 20-inch supersonic wind tunnel using laser-induced thermal acoustics
606   $aMach number$2nasat
606   $aTemperature$2nasat
606   $aFreestream measurement$2nasat
606   $aLaser-induced thermal acoustics (LITA)$2nasat
606   $a20-inch supersonic wind tunnel (SWT)$2nasat
615  7$aMach number.
615  7$aTemperature.
615  7$aFreestream measurement.
615  7$aLaser-induced thermal acoustics (LITA)
615  7$a20-inch supersonic wind tunnel (SWT)
700   $aHerring$b Gregory C.$01394410
702   $aBalla$b R. Jeffrey
702   $aBeeler$b George B.
712 02$aLangley Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910713933803321
996   $aFreestream Mach-number and temperature measurement in NASA Langley's 20-inch supersonic wind tunnel using laser-induced thermal acoustics$93468833
997   $aUNINA