01144nam0-2200373li-450 99000014386020331620180312154800.088-386-0612-90014386USA010014386(ALEPH)000014386USA01001438620001109d1993----km-y0itay0103----baitaITCompatibilità elettromagneticainterferenza e immunità di apparati e sistemiBruno AudoneMilanoMcGraw-Hillcopyr. 1993Sul front: FINMECCANICACompatibilita elettromagnetica621.38224AUDONE,Bruno333475Sistema bibliotecario di Ateneo dell' Università di SalernoRICA990000143860203316621.382 24 AUD0005165621.382 AUD1053 Crd.1053 Crd. $$ 00331764BKTECCRD1995060920001110USA01171220020403USA011622PATRY9020040406USA011611Compatibilità elettromagnetica114113UNISA01853nam 2200517I 450 991070488030332120260430112328.0(CKB)5470000002444929(OCoLC)904623330(DGPO)000908569(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