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100   $a20110929j199704    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aDynamic analysis with stress mode animation by the integrated force method /$fSurya N. Patnaik, Rula M. Coroneos and Dale A. Hopkins
210  1$a[Washington, D.C.] :$cNational Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program,$dApril 1997.
215   $a1 online resource (17 pages) $cillustrations
225 1 $aNASA technical memorandum ;$v4729
300   $aTitle from title screen (viewed Feb. 23, 2016).
300   $a"April 1997."
300   $a"Performing organization: National Aeronautics and Space Administration, Lewis Research Center, Cleveland, Ohio"--Report documentation page.
320   $aIncludes bibliographical references (page 17).
606   $aStress analysis$2nasat
606   $aStructural design$2nasat
606   $aDesign analysis$2nasat
606   $aInternational Space Station$2nasat
606   $aDynamic loads$2nasat
615  7$aStress analysis.
615  7$aStructural design.
615  7$aDesign analysis.
615  7$aInternational Space Station.
615  7$aDynamic loads.
700   $aPatnaik$b Surya N.$0471368
702   $aCoroneos$b Rula M.
702   $aHopkins$b Dale A.
712 02$aLewis Research Center.
712 02$aUnited States.$bNational Aeronautics and Space Administration.$bScientific and Technical Information Program,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCQ
801  2$bOCLCF
801  2$bOCLCO
801  2$bGPO
906   $aBOOK
912   $a9910704398803321
996   $aDynamic analysis with stress mode animation by the integrated force method$93440696
997   $aUNINA