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035   $a(EXLCZ)995470000002528974
100   $a20220211j199802    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aFuel injector patternation evaluation in advanced liquid-fueled, high pressure, gas turbine combustors, using nonintrusive optical diagnostic techniques /$fR.J. Locke [and three others]
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Lewis Research Center,$dFebruary 1998.
215   $a1 online resource (approximately 18 pages) $cillustrations (chiefly color)
225 1 $aNASA/TM ;$v1998-206292
300   $a"February 1998."
300   $a"Prepared for the 1997 JANNAF 34th CS/PSHS/APS Joint Meeting sponsored by the Chemical Propulsion Information Agency West Palm Beach, Florida, October, 1997."
320   $aIncludes bibliographical references (pages 10-11).
606   $aHigh pressure$2nasat
606   $aCombustion$2nasat
606   $aTurbines$2nasat
615  7$aHigh pressure.
615  7$aCombustion.
615  7$aTurbines.
700   $aLocke$b Randy J.$01395069
712 02$aLewis Research Center,
801  0$bGPO
801  1$bGPO
801  2$bGPO
801  2$bOCLCO
801  2$bGPO
906   $aBOOK
912   $a9910717124503321
996   $aFuel injector patternation evaluation in advanced liquid-fueled, high pressure, gas turbine combustors, using nonintrusive optical diagnostic techniques$93547477
997   $aUNINA