LEADER 02420oam  2200589 a 450 
001 9910702001403321
005 20120629125742.0
035   $a(CKB)5470000002422099
035   $a(OCoLC)797176019
035   $a(EXLCZ)995470000002422099
100   $a20120629d1992      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 00$aCombustion of lox with H??g? under subcritical, critical and supercritical conditions (task 1) and experimental observation of dense spray and mixing of impinging jets (task 2)$b[electronic resource] $esemi-annual report /$fprepared by K.K. Kou ... [et al
210  1$aUniversity Park, PA :$cPropulsion Engineering Research Center, Pennsylvania State University ;$aHuntsville, Ala. :$cNASA Marshall Space Flight Center,$d[1992]
215   $a1 online resource (vi, 55 pages) $cillustrations
225 1 $a[NASA contractor report] ;$vNASA-CR-191222
300   $aTitle from title screen (viewed on June 29, 2012).
300   $a"November 1992."
320   $aIncludes bibliographical references (page 35).
517   $aCombustion of lox with H??g? under subcritical, critical and supercritical conditions 
606   $aCavitation flow$2nasat
606   $aCombustion physics$2nasat
606   $aHydrogen$2nasat
606   $aImpingement$2nasat
606   $aLiquid oxygen$2nasat
606   $aMathematical models$2nasat
606   $aSpray characteristics$2nasat
606   $aSprayers$2nasat
606   $aThermodynamic equilibrium$2nasat
615  7$aCavitation flow.
615  7$aCombustion physics.
615  7$aHydrogen.
615  7$aImpingement.
615  7$aLiquid oxygen.
615  7$aMathematical models.
615  7$aSpray characteristics.
615  7$aSprayers.
615  7$aThermodynamic equilibrium.
701   $aKuo$b Kenneth K$013378
712 02$aPennsylvania State University.$bPropulsion Engineering Research Center.
712 02$aGeorge C. Marshall Space Flight Center.
801  0$bGPO
801  1$bGPO
801  2$bGPO
906   $aBOOK
912   $a9910702001403321
996   $aCombustion of lox with H??g? under subcritical, critical and supercritical conditions (task 1) and experimental observation of dense spray and mixing of impinging jets (task 2)$93442739
997   $aUNINA