01699nam 2200481I 450 991070447440332120130617155005.0(CKB)5470000002440949(OCoLC)848927770(EXLCZ)99547000000244094920130617d2012 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierDevelopment and calibration of a system-integrated rotorcraft finite element model for impact scenarios /Martin S. Annett [and four others]Hampton, Virginia :National Aeronautics and Space Administration, Langley Research Center,2012.1 online resource (62 pages) color illustrationsNASA/TM ;2012-217785Title from title screen (viewed on June 17, 2013)."November 2012."Includes bibliographical references (pages 60-62).HelicoptersnasatCrashworthinessnasatImpact loadsnasatFinite element methodnasatCalibratingnasatRotary wing aircraftnasatHelicopters.Crashworthiness.Impact loads.Finite element method.Calibrating.Rotary wing aircraft.Annett Martin S.1403865Langley Research Center,GPOGPOBOOK9910704474403321Development and calibration of a system-integrated rotorcraft finite element model for impact scenarios3477326UNINA