************************** Materials ******************************************* * *[MATPRP] Material definitions: * E ksf Modulus of elasticity. * V Poisson's ratio. * G ksf Shear modulus, if zero computed from E & V. * * Material Name E V G * =============== =====(ksi) ====== =====(ksi) MATPRP STEEL 29000 0.300 11154 MATPRP Very_Low_E 0 0.300 0 ************************** Member Sections ************************************* * * [ELEPRP] Member sections: * Area ft^2 Cross section area in Y-Z plane. * Iyy ft^4 Weak axis bending inertia. * Izz ft^4 Strong axis bending inertia. * Jxy ft^4 Torsional resistance. * * Section Name Area Iyy Izz Jxy * =============== ====(in^2) ====(in^4) ====(in^4) ====(in^4) ELEPRP LM_S1:00:000000 144.000 4624.000 18560.000 23184.000 ELEPRP LM_S2:00:000000 144.000 4624.000 18560.000 23184.000 ************************** Plate Sections ************************************** * * [PLTPRP] Plate Sections: * Thick ft Plate thickness. * * Section Name Thick * =============== ======(in) ************************** Nodes or Joints ************************************* * * [NODE] Nodes or Joints. * Number Node number. * X,Y,Z ft Node location. * X,Y,Z Axial Constraint or Release. * RX,RY,RZ Rotational Constraint or Release. * * NOTE: For contraints, use "R" or "1" to release the node and "C" or "0" * to constrain the node. * * Example constraints: * X Y Z RX RY RZ * = = = = = = * C C C C C C Fixed node. * C C C C C R Pinned in the X-Y plane. * R C C C C R Roller/rail joint in the X-Y plane. * R R C C C R Roller/ball joint. * C C C R R R Fully pinned joint, as in a truss. * * Coordinates -Trans- -Rotate * Num (Name) X Y Z X Y Z X Y Z * ===== =============== ======(ft) ======(ft) ======(ft) = = = = = = NODE 1 0.000 0.000 0.000 C C C C C R NODE 2 50.000 0.000 0.000 R C C C C R NODE 3 100.000 0.000 0.000 R C C C C R ******************************** Members *************************************** * * [MBR] Linear members: * Num Member number. * NodeA Node at beginning of member. * NodeB Node at end of member. * Beta deg Orientation angle of member * Material Name Name of material for member. * Section Name Name of member section for member. * Releases End Release/Constraint for member at each node. * Release code is a binary code: zyxZYX * "zyx" for moment releases. 1=Released * "ZYX" for translation releases. 1=Released * Example: 110000 for a pin end member. * Coupling Identifies unidirectional members. * Use 'T' for Tension, 'C' for Compression, * or 'X' for normal. * Spacing Identifies difference between member length under * load and design length before member is deactivated. * Unidirectional members are deactivated in the * following conditions: * Compression only member: * When the load length minus the design length * is greater than 'Spacing'. * Tension only member: * When the design length minus the load length * is greater than 'Spacing'. * * - Releases - * NodeA NodeB * Member NodeA NodeB Beta Material Name Section Name zyxZYX zyxZYX Length * ====== ===== ===== =(deg) =============== =============== ====== ====== ======== MBR 1 1 2 0.0 STEEL LM_S1:00:000000 000000 000000 50.000 MBR 2 2 3 0.0 STEEL LM_S2:00:000000 000000 000000 50.000 *********************************** Plates ************************************* * * [PLATE] Plate elements: * Num Plate number. * NodeA First node of plate. * NodeB Second node of plate. * NodeC Third node of plate. * NodeD Fourth node of plate. Set to NodeC for triangles. * Material Name Name of material for plate. * Section Name Name of plate section for plate. * * Output data: * Width Width of plate. * Height Height of plate. * * NOTE: The FEM3D modeler only supports triangular or rectangular plates. * * To specify a triangular plate, set NodeD equal to NodeC. * * For rectangular plates, nodes must be identify in order by going along the * perimeter of the plate (i.e. DO NOT go accross the diagonal). Therefore * side A-B must be parallel to D-C, side B-C must be parallel to A-D, and * side A-B must be perpendicular to A-D. * * * Plate NodeA NodeB NodeC NodeD Material Name Section Name * ===== ===== ===== ===== ===== =============== =============== ******************************* Load Cases ************************************* * * [LDCASE] Load Cases: * Define valid load case names. * * Load Case Name * =============== LDCASE DL_1 ****************************** Nodal Loading *********************************** * * [NODELD] Nodal loading: * Load Case Name Name of load case this load belongs to. Load case * must be defined by previous "LDCASE" card. * Node Name of node to apply load to. * Force/Moment Indicates if this is a force or moment. * Magnitude Magnitude of force in kips or moment in * kips per foot. * X,Y,Z Direction of applied load onto node. * (-1.0 in Y direction is normally down) * * Force/Moment -+ * F Magnitude ------- Direction Vector ------- * Load Case Name Node M (k) (k-ft) X Y Z * =============== ===== = ========== ========== ========== ========== ****************************** Member Loading ********************************** * * [MBRLD] Member loading: * Load Case Name Name of load case this load belongs to. Load case * must be defined by previous "LDCASE" card. * Membr Name of member to apply load to. * Force/Moment Indicates if this is a force or moment. * Global/Local Indicates if direction vector is in global or local * coordinate system. * Absolute/Fraction Indicates if distance is absolute distance in feet or * a percentage of the length of the member. * Magnitude Magnitude of force in kips, magnitude of moment in * kips per foot, or beginning magnitude of trapizodial * linear load. * Dist Location of concentrated force/moment or beginning * location of trapizodial linear load. * Dist Zero if concentrated force/moment or ending location * of trapizodial linear load (must be greater than * beginning location). * Magnitude Ending magnitude for trapizodial linear load. Ignored * but must be specified for concentrated force/moment. * X,Y,Z Direction of applied load onto member. * (-1.0 in Y direction is normally down) * * Force/Moment-++-Global/Local * ||+-Absolute/Fraction * ||| * FGA Magnitude Dist Dist Magnitude - Direction Vector - * Load Case Name Membr MLF (k) (k-ft) (ft) (ft) (k) (k-ft) X Y Z * =============== ===== === ========== ======== ======== ========== ====== ====== ====== MBRLD DL_1 1 FGA 0.490 0.00 50.00 0.490 0.000 -1.000 0.000 MBRLD DL_1 2 FGA 0.490 0.00 50.00 0.490 0.000 -1.000 0.000 ***************************** Commands ***************************************** * * Commands: * NOTE: Commands are case insensative except for load case and combination * names. * * COMPUTE * Compute stiffness matrix. * * PRINTMODEL * Instructs FEM 3D Engine to print model definition. * Best done after the COMPUTE command so that the node indexes are * calculated. * * SOLVE * Solve for specified load case or combination with the specified * multiplier. * * EVALNODE * Evaluate specified node and print results. * * EVALALLNODES * Evaluate all nodes and print results. * * EVALMBR * Evaluate specified member and print results. * Number of Divisions default = 11 * * EVALALLMBRS * Evaluate all members and print results. * Number of Divisions default = 11 * * UNI_ANALYSIS * Enable or disbale the Uni-direction member ananlysis. * * ******************************************************************************** Compute PrintModel Solve DL_1 1.000000 EvalAllNodes EvalAllMbrs ========================================== Load case: DL_1 ========================================== **************************** Nodal Results ************************************* * * [NDRES] Nodal Results * * ========== Translation / Rotation ================= ================ Reactions ===================== * Node X Y Z RX RY RZ X Y Z RX RY RZ * (in) (in) (in) (rad) (rad) (rad) (kip) (kip) (kip) (k-ft) (k-ft) (k-ft) * ===== ======== ======== ======= ======== ======== ======== ======== ======== ======= ======== ======== ======== NDRES 1 0.000 0.000 0.000 0.000 0.000 -0.000 0.000 9.188 0.000 0.000 0.000 0.000 NDRES 2 0.000 0.000 0.000 0.000 0.000 0.000 0.000 30.625 0.000 0.000 0.000 0.000 NDRES 3 0.000 0.000 0.000 0.000 0.000 0.000 0.000 9.188 0.000 0.000 0.000 0.000 ========================================== Load case: DL_1 ========================================== **************************** Member Results ************************************* * * [MBRRES] Member Results * * ============== Major Axis ======== ============= Minor Axis ========== * Dist Axial Moment LftShear RtShear Disp Moment LftShear RtShear Disp * Mbr (ft) (kip) (k-ft) (kip) (kip) (in) (k-ft) (kip) (kip) (in) * ===== == ========== ======== ======== ======== ======== ======== ======== ======== ======== ======== MBRRES 1 1 0.000 0.00 0.00 9.19 9.19 0.0000 0.00 0.00 0.00 0.0000 MBRRES 1 2 5.000 0.00 -39.81 6.74 6.74 -0.0195 0.00 0.00 0.00 0.0000 MBRRES 1 3 10.000 0.00 -67.38 4.29 4.29 -0.0361 0.00 0.00 0.00 0.0000 MBRRES 1 4 15.000 0.00 -82.69 1.84 1.84 -0.0473 0.00 0.00 0.00 0.0000 MBRRES 1 5 20.000 0.00 -85.75 -0.61 -0.61 -0.0521 0.00 0.00 0.00 0.0000 MBRRES 1 6 25.000 0.00 -76.56 -3.06 -3.06 -0.0502 0.00 0.00 0.00 0.0000 MBRRES 1 7 30.000 0.00 -55.12 -5.51 -5.51 -0.0423 0.00 0.00 0.00 0.0000 MBRRES 1 8 35.000 0.00 -21.44 -7.96 -7.96 -0.0301 0.00 0.00 0.00 0.0000 MBRRES 1 9 40.000 0.00 24.50 -10.41 -10.41 -0.0164 0.00 0.00 0.00 0.0000 MBRRES 1 10 45.000 0.00 82.69 -12.86 -12.86 -0.0048 0.00 0.00 0.00 0.0000 MBRRES 1 11 50.000 0.00 153.12 -15.31 -15.31 0.0000 0.00 0.00 0.00 0.0000 MBRRES 2 1 0.000 0.00 153.12 15.31 15.31 0.0000 0.00 0.00 0.00 0.0000 MBRRES 2 2 5.000 0.00 82.69 12.86 12.86 -0.0048 0.00 0.00 0.00 0.0000 MBRRES 2 3 10.000 0.00 24.50 10.41 10.41 -0.0164 0.00 0.00 0.00 0.0000 MBRRES 2 4 15.000 0.00 -21.44 7.96 7.96 -0.0301 0.00 0.00 0.00 0.0000 MBRRES 2 5 20.000 0.00 -55.12 5.51 5.51 -0.0423 0.00 0.00 0.00 0.0000 MBRRES 2 6 25.000 0.00 -76.56 3.06 3.06 -0.0502 0.00 0.00 0.00 0.0000 MBRRES 2 7 30.000 0.00 -85.75 0.61 0.61 -0.0521 0.00 0.00 0.00 0.0000 MBRRES 2 8 35.000 0.00 -82.69 -1.84 -1.84 -0.0473 0.00 0.00 0.00 0.0000 MBRRES 2 9 40.000 0.00 -67.38 -4.29 -4.29 -0.0361 0.00 0.00 0.00 0.0000 MBRRES 2 10 45.000 0.00 -39.81 -6.74 -6.74 -0.0195 0.00 0.00 0.00 0.0000 MBRRES 2 11 50.000 0.00 0.00 -9.19 -9.19 0.0000 0.00 0.00 0.00 0.0000