LEADER 01938oam  2200589Ia 450 
001 9910700166803321
005 20110224103204.0
035   $a(CKB)5470000002407297
035   $a(OCoLC)703593465
035   $a(EXLCZ)995470000002407297
100   $a20110224d1984      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aBurner liner thermal/structural load modeling$b[electronic resource] /$fby R. Maffeo
210  1$aCincinnati, OH :$cGeneral Electric Co., Aircraft Engine Business Group,$d[1984]
215   $a1 online resource (iii, 203 pages) $cdigital, PDF file
225 1 $a[NASA] CR ;$v174892
300   $aTitle from title screen (viewed Feb. 23, 2011).
300   $a"October 1984"--Rept. doc. p.
300   $a"Prepared for National Aeronautics and Space Administration, Lewis Research Center."
320   $aIncludes bibliographical references (page 203).
606   $aBurners$2nasat
606   $aCombustion chambers$2nasat
606   $aComputer aided design$2nasat
606   $aHeat transfer$2nasat
606   $aInterfaces$2nasat
606   $aLinings$2nasat
606   $aLoads (forces)$2nasat
606   $aStress analysis$2nasat
606   $aTemperature distribution$2nasat
615  7$aBurners.
615  7$aCombustion chambers.
615  7$aComputer aided design.
615  7$aHeat transfer.
615  7$aInterfaces.
615  7$aLinings.
615  7$aLoads (forces)
615  7$aStress analysis.
615  7$aTemperature distribution.
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
801  2$bGPO
906   $aBOOK
912   $a9910700166803321
996   $aBurner liner thermal$93481004
997   $aUNINA