LEADER 01779nam  2200505I  450 
001 9910704816803321
005 20131113164317.0
035   $a(CKB)5470000002445571
035   $a(OCoLC)862949255
035   $a(EXLCZ)995470000002445571
100   $a20131113d2013      ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aAdvanced shock position control for mode transition in a turbine based combined cycle engine inlet model /$fJeffrey T. Csank and Thomas J. Stueber
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$d[2013]
215   $a1 online resource (12 pages) $cillustrations
225 1 $aNASA/TM ;$v2013-216515
300   $aTitle from title screen (viewed Nov. 13, 2013).
300   $a"May 2013."
320   $aIncludes bibliographical references (pages 11-12).
606   $aInlet flow$2nasat
606   $aControllers$2nasat
606   $aFeedback control$2nasat
606   $aComputerized simulation$2nasat
606   $aTurbine engines$2nasat
606   $aEngine inlets$2nasat
615  7$aInlet flow.
615  7$aControllers.
615  7$aFeedback control.
615  7$aComputerized simulation.
615  7$aTurbine engines.
615  7$aEngine inlets.
700   $aCsank$b Jeffrey T.$01402819
702   $aStueber$b Thomas J.
712 02$aFundamental Aeronautics Program (U.S.),
712 02$aNASA Glenn Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910704816803321
996   $aAdvanced shock position control for mode transition in a turbine based combined cycle engine inlet model$93512465
997   $aUNINA