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035   $a(CKB)5470000002434442
035   $a(OCoLC)916511222
035   $a(EXLCZ)995470000002434442
100   $a20150807j201501    ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aWing shape sensing from measured strain /$fChan-gi Pak
210  1$aEdwards, CA :$cNational Aeronautics and Space Administration Armstrong Flight Research Center,$dJanuary 2015.
215   $a1 online resource (27 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2015-218358
300   $aTitle from title screen (viewed Aug. 7, 2015).
300   $a"January 2015."
320   $aIncludes bibliographical references (page 27).
606   $aAircraft structures$2nasat
606   $aAerodynamic loads$2nasat
606   $aFinite element method$2nasat
606   $aStrain measurement$2nasat
606   $aLeast squares method$2nasat
615  7$aAircraft structures.
615  7$aAerodynamic loads.
615  7$aFinite element method.
615  7$aStrain measurement.
615  7$aLeast squares method.
700   $aPak$b Chan-gi$01386346
712 02$aNASA Neil A. Armstrong Flight Research Center,
712 02$aFundamental Aeronautics Program (U.S.)
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910703728203321
996   $aWing shape sensing from measured strain$93502363
997   $aUNINA