please set up boundary conditions do not solve the whole problem format it in MATLAB if possible Here is the node inform

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answerhappygod
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please set up boundary conditions do not solve the whole problem format it in MATLAB if possible Here is the node inform

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please set up boundary conditions do not solve the whole problem format it in MATLAB if possible
Please Set Up Boundary Conditions Do Not Solve The Whole Problem Format It In Matlab If Possible Here Is The Node Inform 1
Please Set Up Boundary Conditions Do Not Solve The Whole Problem Format It In Matlab If Possible Here Is The Node Inform 1 (31.53 KiB) Viewed 38 times
Please Set Up Boundary Conditions Do Not Solve The Whole Problem Format It In Matlab If Possible Here Is The Node Inform 2
Please Set Up Boundary Conditions Do Not Solve The Whole Problem Format It In Matlab If Possible Here Is The Node Inform 2 (34.91 KiB) Viewed 38 times
Here is the node information:
Please Set Up Boundary Conditions Do Not Solve The Whole Problem Format It In Matlab If Possible Here Is The Node Inform 3
Please Set Up Boundary Conditions Do Not Solve The Whole Problem Format It In Matlab If Possible Here Is The Node Inform 3 (30.65 KiB) Viewed 38 times
Please Set Up Boundary Conditions Do Not Solve The Whole Problem Format It In Matlab If Possible Here Is The Node Inform 4
Please Set Up Boundary Conditions Do Not Solve The Whole Problem Format It In Matlab If Possible Here Is The Node Inform 4 (27.32 KiB) Viewed 38 times
L LL D 212 P P P Figure 2: Idealized Truss Geometry The half weight of each passenger car is P = 2 k. The member spacing is L = 20 ft. The cross section of each truss member is constant and shown in Figure 2 above. Each truss member is made of A992 steel, which has E = 29,000 ksi. L ONL 4 F
From line 45 to 47, you need to put the boundary conditions (known dofs). The displacement is denoted by u (16X1 vector). Similar to the load vector, input your DOF number in the bracket and enter the known displacement value. There are 3 values you need to input. Note that you need to follow closely to the numbering system in section 1. u( )= u( )= u( )= After defining your member stiffness matrix, applied load vector and known dofs, you can press run and the code will give you the nodal force and displacement.
Node information: For each member, the near nodes and far nodes are summarized in the following table. Member Near Node Far Node 1 1 2 2 2 3 3 3 4 4 4 5 1 6 2 6 3 6 3 7 3 8 4 8 8 7 8 5 6 7 8 9 10 11 12 13 23 456 7
DOF numbering: For each node, there are two DOFs: displacement in x and y. The DOF number for each node is listed below. Note that this numbering system is different from what we usually do in class (Unknown DOF first then Known DOF). We assign the DOF from lower node to higher node for simplicity of the assembly process. Node DOF (x displacement) DOF (y displacement) 1 1 2 2 3 4 5 6 7 8 10 12 14 16 3 45678 9 11 13 15
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