LEADER 01727oam  2200469I  450 
001 9910713590403321
005 20200925144444.0
035   $a(CKB)5470000002501756
035   $a(OCoLC)1153938334
035   $a(OCoLC)995470000002501756
035   $a(EXLCZ)995470000002501756
100   $a20200511j202004    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aCombustion dynamics characteristics and fuel pressure modulation responses of a three-cup third-generation swirl-venturi lean direct injection combustion concept /$fZhuohui J. He [and five others]
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$dApril 2020.
215   $a1 online resource (9 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2020-220522
300   $a"April 2020."
320   $aIncludes bibliographical references (page 9).
606   $aFuel injection$2nasat
606   $aCombustion$2nasat
606   $aCombustion chambers$2nasat
606   $aNoise measurement$2nasat
606   $aFuel-air ratio$2nasat
615  7$aFuel injection.
615  7$aCombustion.
615  7$aCombustion chambers.
615  7$aNoise measurement.
615  7$aFuel-air ratio.
700   $aHe$b Zhuohui J.$01403836
712 02$aNASA Glenn Research Center,
801  0$bGPO
801  1$bGPO
801  2$bGPO
906   $aBOOK
912   $a9910713590403321
996   $aCombustion dynamics characteristics and fuel pressure modulation responses of a three-cup third-generation swirl-venturi lean direct injection combustion concept$93477247
997   $aUNINA