LEADER 01819nam  2200505Ia 450 
001 9910700183403321
005 20110216134723.0
035   $a(CKB)5470000002407129
035   $a(OCoLC)702135109
035   $a(EXLCZ)995470000002407129
100   $a20110216d1985      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aBurner liner thermal/structural load modeling$b[electronic resource] $eTRANCITS program user's manual /$fby R. Maffeo
210  1$aCincinnati, OH :$cGeneral Electric Co., Aircraft Engine Business Group,$d[1985]
215   $a1 online resource (iii, 44 pages) $cdigital, PDF file
225 1 $a[NASA] CR ;$v174891
300   $aTitle from title screen (viewed Feb. 15, 2011).
300   $a"August 1985."
300   $aPrepared for National Aeronautics and Space Administration, Lewis Research Center.
517   $aBurner liner thermal/structural load modeling 
606   $aComputer aided design$2nasat
606   $aDynamic models$2nasat
606   $aDynamic structural analysis$2nasat
606   $aIsoparametric finite elements$2nasat
606   $aLoads (forces)$2nasat
606   $aUser manuals (computer programs)$2nasat
615  7$aComputer aided design.
615  7$aDynamic models.
615  7$aDynamic structural analysis.
615  7$aIsoparametric finite elements.
615  7$aLoads (forces)
615  7$aUser manuals (computer programs)
700   $aMaffeo$b R$01405093
712 02$aGeneral Electric Company.$bAircraft Engine Business Group.
712 02$aLewis Research Center.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910700183403321
996   $aBurner liner thermal$93481004
997   $aUNINA