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1 PLANE FRAME AND TRUSS ANALYSIS
STRUCTURE DATA FOR JOB IDENT. EXAMPLE1
MEM= 2 NJ= 3 NLD= 1 E= 3000000.
JOINT COORDINATES
JOINT JRF JVF JHF X-COORDINATE Y-COORDINATE
1 1 1 1 0.000 5.000
2 0 0 0 0.000 0.000
3 1 1 1 5.000 0.000
1 MEMBER DATA
MEM NO J K INERTIA AREA MODULUS LENGTH TYPE SPRINGTYPE VALUE K VALUE
0 1 1 2 0.1000E-03 0.1000E-05 3000000.110 5.000 1 0 0. 0.0000E+00
0 2 2 3 0.1000E-03 0.1000E-05 3000000.110 5.000 0 0 0. 0.0000E+00
1 INPUT DATA FOR LOADING NUMBER 1
MEMBER LOAD BEGIN LOAD END X BEGIN X END ALPHA
1 0.500 0.000 0.000 5.000 0.000
0 JOINT DEFLECTIONS AND ROTATIONS FOR LOADING 1
J ROTATION VERT DEFL HORZ DEFL
1 0.00000000E+00 0.00000000E+00 0.00000000E+00
2 -0.24084046E-01-0.58981335E-01 0.18327252E+00
3 0.00000000E+00 0.00000000E+00 0.00000000E+00
1 BEAM MOMENTS AND SHEARS LOADING 1
J MOMENT K MOMENT J SHEAR K SHEAR J AXIAL K AXIAL
MEMBER NO. 1 0.0000E+00 0.1534E+01 -0.1140E+01 -0.1100E+00 -0.3539E-01 0.3539E-01
MEMBER NO. 2 -0.1534E+01 0.1357E+01 0.3539E-01 -0.3539E-01 0.1100E+00 -0.1100E+00
1 INFLUENCE LINE OF DEFLECTION CURVE
0.0000000E+00
0 INFLUENCE LINE OF B.M.
MEM= 1
0.1533516E+01
MEM= 2
0.1356570E+01
0 INFLUENCE LINE OF S.F.
-0.1099635E+00
-0.3538900E-01
0 INFLUENCE LINE OF A.F.
0.3538880E-01
-0.1099635E+00