>> Plane_Frame Read 3 nodes. Node, BC_Flag, Coordinates 1 111 0 120 0 2 000 120 120 0 3 010 120 0 0 Read 2 elements. Elem, Type, Connectivity_List 1 1 1 2 2 1 2 3 Maximum element type number = 1 Read 4 essential boundary condition sets. Node DOF Value_EBC 1 1 0 1 2 0 1 3 0 3 2 0 Option = 3 % <<-- manually set line loads Application properties are: Cross-sectional area = 10 Elastity modulus = 3e+07 Mass density = 110 Moment of inertia = 100 Element number 1 Line Load = [ -83.333 -83.333 ] p_to_F = 0 0 42 18 720 480 0 0 18 42 -480 -720 Local s_L = 1.0e+08 * 0.0250 0 0 -0.0250 0 0 0 0.0002 0.0125 0 -0.0002 0.0125 0 0.0125 1.0000 0 -0.0125 0.5000 -0.0250 0 0 0.0250 0 0 0 -0.0002 -0.0125 0 0.0002 -0.0125 0 0.0125 0.5000 0 -0.0125 1.0000 Local c_L = 1.0e+04 *[ 0 -0.5000 -10.0000 0 -0.5000 10.0000] Local t_L = 1 0 0 0 0 0 0 1 0 0 0 0 0 0 1 0 0 0 0 0 0 1 0 0 0 0 0 0 1 0 0 0 0 0 0 1 Global S_e = 1.0e+08 * 0.0250 0 0 -0.0250 0 0 0 0.0002 0.0125 0 -0.0002 0.0125 0 0.0125 1.0000 0 -0.0125 0.5000 -0.0250 0 0 0.0250 0 0 0 -0.0002 -0.0125 0 0.0002 -0.0125 0 0.0125 0.5000 0 -0.0125 1.0000 Global C_e = 1.0e+04 *[ 0 -0.5000 -10.0000 0 -0.5000 10.0000] Element number 2 Line Load = [ 0 0 ] Local s_L = 1.0e+08 * 0.0250 0 0 -0.0250 0 0 0 0.0002 0.0125 0 -0.0002 0.0125 0 0.0125 1.0000 0 -0.0125 0.5000 -0.0250 0 0 0.0250 0 0 0 -0.0002 -0.0125 0 0.0002 -0.0125 0 0.0125 0.5000 0 -0.0125 1.0000 Local c_L = 0 0 0 0 0 0 Local t_L = 0 -1 0 0 0 0 1 0 0 0 0 0 0 0 1 0 0 0 0 0 0 0 -1 0 0 0 0 1 0 0 0 0 0 0 0 1 Global S_e = 1.0e+08 * 0.0002 0 0.0125 -0.0002 0 0.0125 0 0.0250 0 0 -0.0250 0 0.0125 0 1.0000 -0.0125 0 0.5000 -0.0002 0 -0.0125 0.0002 0 -0.0125 0 -0.0250 0 0 0.0250 0 0.0125 0 0.5000 -0.0125 0 1.0000 Global C_e = 0 0 0 0 0 0 Global S = 1.0e+08 * Columns 1 through 7 0.0250 0 0 -0.0250 0 0 0 0 0.0002 0.0125 0 -0.0002 0.0125 0 0 0.0125 1.0000 0 -0.0125 0.5000 0 -0.0250 0 0 0.0252 0 0.0125 -0.0002 0 -0.0002 -0.0125 0 0.0252 -0.0125 0 0 0.0125 0.5000 0.0125 -0.0125 2.0000 -0.0125 0 0 0 -0.0002 0 -0.0125 0.0002 0 0 0 0 -0.0250 0 0 0 0 0 0.0125 0 0.5000 -0.0125 Columns 8 through 9 0 0 0 0 0 0 0 0.0125 -0.0250 0 0 0.5000 0 -0.0125 0.0250 0 0 1.0000 Global C = 1.0e+04 *[ 0 -0.5000 -10.0000 0 -0.5000 10.0000 0 0 0] ====== SOLUTION ======== Node, DOF, Resultant input sources 1 2 -4999.98 1 3 -99999.6 2 2 -4999.98 2 3 99999.6 3 DOF Totals = 1.0e+03 * [ 0 -10.0000 0] Computed nodal displacements at 3 nodes Node DOF_1 DOF_2 DOF_3 1 0 0 0 2 -1.39852e-19 -0.00149688 0.000981285 3 0.117754 0 0.000981285 Recovered 4 System Reactions Node, DOF, Value of reaction 1 1 3.4963e-13 1 2 6257.77 1 3 150935 3 2 3742.19 3 DOF Totals = 1.0e+05 * [ 0.0000 0.1000 1.5093] % THINK about the moment ---------------------^ >> quit