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Problem 2 [Required]: For the truss below (and using the Stiffness Method): (a) Determine the global stiffness matrix; (b) Ca
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Soution 23 s S uso 2 EN Node anes Hout Membeeig Member of Truss » tu, Elementl: 0= 180t45 L=12 m . Nodal print No. - 2 -3 = 2Elenent 3: o = 180°+90 L=am Nocal points 1-4 ! 31 = EA loo ool1 loi 0-12 as 220° = 0 Sim270= -1 1-3 EA Elementu: 0 = 360°-45Global mateix if of 868 2 3 u s 6 7 8 -1/31-1101-1/2 1/2010 ] 12 12010112 Tk] = EA Pol 3/2 1/2-1/2-1/2 bol 1/2 - 1/2 +/2-1/2o o Г - o o o] Го 7 г. o o oo) – Ч. 2 1:2 о - 2 | е о то | о о г - о| По Но о то о с 2 - 2 1 - чо | | o . ч.ч. о. 8 9 o о o |Now calculate individual member forces Member I. e=r2m mals l=-1152 [p] = [go to ton] Thor] us = AE [ z f t t 534) EA -- +4.2Members 21 taza szara. Scanned with CamScanner

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