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STRUCTURAL ANALYSIS <br /> <br />*** NOOAL DISPLACEMENT (IN GLOBAL COORDINATEB) <br /> <br />NODE <br /> <br />* .......... TRANSLATION .......... <br /> DX DY <br /> <br />* ....... ROTATION (BADIAN) ....... <br /> OX OY <br /> <br />1.190E~03 <br />-2.379E-03 <br />-2.606E-0'5 <br />-2.628E-03 <br />-3,46~E-03 <br />-4.676E-O& <br /> <br /> &~694E-04 <br /> 3.~82E-03 <br /> <br /> 1.019E-03 <br /> <br />SUPPORT REACTION (IN GLOBAL COORDINATES) <br /> <br />NODE <br /> <br />* ........ REACT[ON FORCE ........ * <br /> RX RY RZ <br /> <br />1 368.01 1256.56 <br />2 -1020.64 .00 <br />12 -760.84 .00 <br />13 315.16 1182.81 <br /> <br />w ....... REACT[ON HO~ENT ........ <br /> MX MY MZ <br /> <br />.00 <br /> <br />.00 <br />.00 <br />.00 <br /> <br />*** NODAL FORCE (IN LOCAL COORDINATES) <br /> <br />ELEMENT NODE * .... SHEAR AND AXIAL FORCE ---* <br /> <br /> PX PY PZ <br /> <br />1 ' 2 1 1256_56 <br />1 ~ 2 2 -1256.56 368.01 <br /> <br />1256.56 652.63 <br />-1256.56 3~7.73 <br /> <br />-.01 1lO.B1 <br />.01 .03 <br /> <br />*- BENDING & TORSIONAL MONENT -* <br /> MX MY NZ <br /> <br /> .00 <br />- 17664.61 <br /> <br />17664.61 <br /> -660.17 <br /> <br />660.;~5 <br /> - .04 <br /> <br />13 - 12 13 1182.81 -315.16 -00 <br />13 - 12 12 -1182.81 315.16 -151Z7.91 <br /> <br /> <br />