LEADER 01699nam  2200481I  450 
001 9910704474403321
005 20130617155005.0
035   $a(CKB)5470000002440949
035   $a(OCoLC)848927770
035   $a(EXLCZ)995470000002440949
100   $a20130617d2012      ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aDevelopment and calibration of a system-integrated rotorcraft finite element model for impact scenarios /$fMartin S. Annett [and four others]
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$d2012.
215   $a1 online resource (62 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2012-217785
300   $aTitle from title screen (viewed on June 17, 2013).
300   $a"November 2012."
320   $aIncludes bibliographical references (pages 60-62).
606   $aHelicopters$2nasat
606   $aCrashworthiness$2nasat
606   $aImpact loads$2nasat
606   $aFinite element method$2nasat
606   $aCalibrating$2nasat
606   $aRotary wing aircraft$2nasat
615  7$aHelicopters.
615  7$aCrashworthiness.
615  7$aImpact loads.
615  7$aFinite element method.
615  7$aCalibrating.
615  7$aRotary wing aircraft.
700   $aAnnett$b Martin S.$01403865
712 02$aLangley Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910704474403321
996   $aDevelopment and calibration of a system-integrated rotorcraft finite element model for impact scenarios$93477326
997   $aUNINA