LEADER 01658nam  2200481I  450 
001 9910703633403321
005 20150825155039.0
035   $a(CKB)5470000002433379
035   $a(OCoLC)919175383
035   $a(EXLCZ)995470000002433379
100   $a20150825j201502    ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aDesign concepts for cooled ceramic composite turbine vane /$fRobert J. Boyle, Ankur H. Parikh, and Vinod K. Nagpal
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$dFebruary 2015.
215   $a1 online resource (iii, 99 pages) $ccolor illustrations
225 1 $aNASA/CR ;$v2015-218390
300   $aTitle from title screen (viewed Aug. 25, 2015).
300   $a"February 2015."
320   $aIncludes bibliographical references (pages 97-99).
606   $aTurboshafts$2nasat
606   $aCeramic matrix composites$2nasat
606   $aTurbofan engines$2nasat
606   $aTurbine blades$2nasat
606   $aPressure distribution$2nasat
615  7$aTurboshafts.
615  7$aCeramic matrix composites.
615  7$aTurbofan engines.
615  7$aTurbine blades.
615  7$aPressure distribution.
700   $aBoyle$b Robert J.$01387461
702   $aParikh$b Ankur H.
702   $aNagpal$b V$g(Vinod),
712 02$aNASA Glenn Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910703633403321
996   $aDesign concepts for cooled ceramic composite turbine vane$93437324
997   $aUNINA