01825nam 2200505I 450 991070488030332120150310165229.0(CKB)5470000002444929(OCoLC)904623330(EXLCZ)99547000000244492920150310j201304 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierMethod for estimating operational loads on aerospace structures using span-wisely distributed surface strains /William L. Ko and Van Tran FleischerEdwards, CA :National Aeronautics and Space Administration, Dryden Flight Research Center,April 2013.1 online resource (vi, 64 pages) illustrationsNASA/TP ;2013-216518Title from title screen (viewed March 10, 2015)."April 2013.""[U.S. Patent-7,715,994]."Includes bibliographical references (page 64).Strain distributionnasatDisplacementnasatLoads (forces)nasatAircraft structuresnasatFinite element methodnasatStructural stabilitynasatStrain distribution.Displacement.Loads (forces)Aircraft structures.Finite element method.Structural stability.Ko William L.1388928Fleischer Van TranNASA Dryden Flight Research Center,GPOGPOBOOK9910704880303321Method for estimating operational loads on aerospace structures using span-wisely distributed surface strains3443878UNINA