LEADER 02167nam  2200553I  450 
001 9910702486003321
005 20130128091620.0
035   $a(CKB)5470000002427305
035   $a(OCoLC)825550608
035   $a(EXLCZ)995470000002427305
100   $a20130128d2012      ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 12$aA turbine based combined cycle engine inlet model and mode transition simulation based on HiTECC tool /$fJeffrey T. Csank and Thomas J. Stueber
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$d2012.
215   $a1 online resource (13 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2012-217714
300   $aTitle from title screen (viewed on Jan. 14, 2013).
300   $a"September 2012."
300   $a"Prepared for the 48th Joint Propulsion Conference and Exhibit cosponsored by AIAA, ASME, SAE, and ASEE Atlanta, Georgia, July 30 to August 1, 2012."
300   $a"AIAA-2012-4149."
320   $aIncludes bibliographical references (pages 12-13).
606   $aComputerized simulation$2nasat
606   $aPropulsion system configurations$2nasat
606   $aWind tunnel tests$2nasat
606   $aFuel systems$2nasat
606   $aPropulsion system performance$2nasat
606   $aTurbine engines$2nasat
606   $aEngine inlets$2nasat
615  7$aComputerized simulation.
615  7$aPropulsion system configurations.
615  7$aWind tunnel tests.
615  7$aFuel systems.
615  7$aPropulsion system performance.
615  7$aTurbine engines.
615  7$aEngine inlets.
700   $aCsank$b Jeffrey T.$01402819
702   $aStueber$b Thomas J.
712 02$aNASA Glenn Research Center,
712 12$aJoint Propulsion Conference and Exhibit$d(48th :$f2012 :$eAtlanta, Ga.)
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910702486003321
996   $aA turbine based combined cycle engine inlet model and mode transition simulation based on HiTECC tool$93489481
997   $aUNINA