LEADER 02052oam  2200529   450 
001 9910707027003321
005 20160330150846.0
035   $a(CKB)5470000002461220
035   $a(OCoLC)755259956
035   $a(EXLCZ)995470000002461220
100   $a20111002j199706    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aFinite-element analysis of a Mach-8 flight test article using nonlinear contact elements /$fW. Lance Richards
210  1$a[Washington, D.C.] :$cNational Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program,$dJune 1997.
215   $a1 online resource (14 pages) $cillustrations
225 1 $aNASA technical memorandum ;$v4796
300   $aTitle from title screen (viewed March 30, 2016).
300   $a"June 1997."
300   $a"Performing organization: NASA Dryden Flight Research Center, Edwards, California"--Report documentation page.
320   $aIncludes bibliographical references (page 14).
606   $aFinite element method$2nasat
606   $aHypersonic speed$2nasat
606   $aStructural design$2nasat
606   $aHypersonic flight$2nasat
606   $aNonlinearity$2nasat
615  7$aFinite element method.
615  7$aHypersonic speed.
615  7$aStructural design.
615  7$aHypersonic flight.
615  7$aNonlinearity.
700   $aRichards$b W. Lance$01399318
712 02$aNASA Dryden Flight 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$bOCLCO
801  2$bGPO
906   $aBOOK
912   $a9910707027003321
996   $aFinite-element analysis of a Mach-8 flight test article using nonlinear contact elements$93464298
997   $aUNINA