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035   $a(OCoLC)904623330
035   $a(EXLCZ)995470000002444929
100   $a20150310j201304    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aMethod for estimating operational loads on aerospace structures using span-wisely distributed surface strains /$fWilliam L. Ko and Van Tran Fleischer
210  1$aEdwards, CA :$cNational Aeronautics and Space Administration, Dryden Flight Research Center,$dApril 2013.
215   $a1 online resource (vi, 64 pages) $cillustrations
225 1 $aNASA/TP ;$v2013-216518
300   $aTitle from title screen (viewed March 10, 2015).
300   $a"April 2013."
300   $a"[U.S. Patent-7,715,994]."
320   $aIncludes bibliographical references (page 64).
606   $aStrain distribution$2nasat
606   $aDisplacement$2nasat
606   $aLoads (forces)$2nasat
606   $aAircraft structures$2nasat
606   $aFinite element method$2nasat
606   $aStructural stability$2nasat
615  7$aStrain distribution.
615  7$aDisplacement.
615  7$aLoads (forces)
615  7$aAircraft structures.
615  7$aFinite element method.
615  7$aStructural stability.
700   $aKo$b William L.$01388928
702   $aFleischer$b Van Tran
712 02$aNASA Dryden Flight Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910704880303321
996   $aMethod for estimating operational loads on aerospace structures using span-wisely distributed surface strains$93443878
997   $aUNINA