LEADER 01831nam  2200517Ia 450 
001 9910697196403321
005 20230902161729.0
035   $a(CKB)5470000002384944
035   $a(OCoLC)647998122
035   $a(EXLCZ)995470000002384944
100   $a20100715d2005      ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 00$aFluids and combustion facility$b[electronic resource] $efluids integrated rack modal model correlation /$fMark E. McNelis ... [and others]
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$d[2005]
215   $a1 online resource (iii, 96 pages) $cillustrations
225 1 $aNASA TM- ;$v2005-214056
300   $aTitle from title screen (viewed on July 15, 2010).
300   $a"December 2005."
300   $a"GRC-DEV-FCF-2005-002."
320   $aIncludes bibliographical references (page 42).
410  0$aNASA technical memorandum ;$v2005-214056.
517   $aFluids and combustion facility 
606   $aInternational Space Station$2nasat
606   $aFinite element method$2nasat
606   $aCombustion chambers$2nasat
606   $aFluid management$2nasat
606   $aVibration mode$2nasat
606   $aDynamic structural analysis$2nasat
615  7$aInternational Space Station.
615  7$aFinite element method.
615  7$aCombustion chambers.
615  7$aFluid management.
615  7$aVibration mode.
615  7$aDynamic structural analysis.
701   $aMcNelis$b Mark E$01386392
712 02$aNASA Glenn Research Center.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910697196403321
996   $aFluids and combustion facility$93435287
997   $aUNINA