LEADER 01850nam  2200445I  450 
001 9910708614403321
005 20170421104802.0
035   $a(CKB)5470000002471086
035   $a(OCoLC)983463186
035   $a(EXLCZ)995470000002471086
100   $a20170421j200207    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aMeasurement and computation of supersonic flow in a lobed diffuser-mixer for trapped vortex combustors /$fAndreja Brankovic [and nine others]
210  1$aCleveland Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$dJuly 2002.
215   $a1 online resource (41 pages) $cillustrations
225 1 $aNASA/TM ;$v2002-211127
300   $a"July 2002."
300   $a"Prepared for the 2001 19th International Congress on Instrumentation in Aerospace Simulation Facilities (ICIASF 2001) cosponsored by IEEE, AES, NASA Glenn, and OAI, Cleveland, Ohio, August 27-30, 2001."
300   $a"Performing organization: National Aeronautics and Space Administration, John H. Glenn Research Center at Lewis Field" Report documentation page.
320   $aIncludes bibliographical references (pages 41).
606   $aCombustion chambers$2nasat
606   $aLobe mixer$2nasat
606   $aSupersonic flow$2nasat
606   $aPitot tubes$2nasat
615  7$aCombustion chambers.
615  7$aLobe mixer.
615  7$aSupersonic flow.
615  7$aPitot tubes.
700   $aBrankovic$b Andreja$01405812
712 02$aNASA Glenn Research Center.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910708614403321
996   $aMeasurement and computation of supersonic flow in a lobed diffuser-mixer for trapped vortex combustors$93483052
997   $aUNINA