LEADER 01961nam  2200505I  450 
001 9910702673303321
005 20141029092358.0
035   $a(CKB)5470000002429454
035   $a(OCoLC)893975091
035   $a(EXLCZ)995470000002429454
100   $a20141029j201405    ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aCFD analysis of flexible thermal protection system shear configuration testing in the LCAT facility /$fPaul G. Ferlemann
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dMay 2014.
215   $a1 online resource (67 pages) $ccolor illustrations
225 1 $aNASA/CR ;$v2014-218258
300   $aTitle from title screen (viewed Oct. 27, 2014).
300   $a"May 2014."
320   $aIncludes bibliographical references (page 67).
517 1 $aComputational fluid dynamics analysis of flexible thermal protection system shear configuration testing in the Large Core Arc Tunnel facility
606   $aComputational fluid dynamics$2nasat
606   $aThermal protection$2nasat
606   $aTest facilities$2nasat
606   $aFlight simulation$2nasat
606   $aAnalysis (mathematics)$2nasat
606   $aSystems engineering$2nasat
615  7$aComputational fluid dynamics.
615  7$aThermal protection.
615  7$aTest facilities.
615  7$aFlight simulation.
615  7$aAnalysis (mathematics)
615  7$aSystems engineering.
700   $aFerlemann$b Paul G.$01393497
712 02$aLangley Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910702673303321
996   $aCFD analysis of flexible thermal protection system shear configuration testing in the LCAT facility$93449686
997   $aUNINA