Assuming to have an input file describing a generic assemblage of beams in, e.g., the following form: Element number I Node i I Node j Elem. Area I Elem Inertia IEILIO 1 1 A1 E1 L1 01 2 1 A2 12 E2 L2...


Assuming to have an input file describing a generic assemblage of beams in,<br>e.g., the following form:<br>Element number I Node i I Node j<br>Elem. Area I Elem Inertia IEILIO<br>1<br>1<br>A1<br>E1 L1 01<br>2<br>1<br>A2<br>12<br>E2 L2 02<br>3<br>3<br>4<br>АЗ<br>13<br>E3 L3<br>ӨЗ<br>N<br>k<br>AN<br>IN<br>EN LN ON<br>and<br>Node num I Nodal Displ u I Nodal Displ v I Nodal rot O | BC Fx | BC Fy | BC M |<br>1<br>1<br>1<br>F1y<br>1<br>2<br>1<br>1<br>F2x<br>1<br>M2<br>3<br>1<br>1<br>M3<br>N<br>1<br>1<br>1<br>FNx<br>FNy<br>MN<br>* 1-> unknown<br>write a code in your preferred computer language or environment (e.g. Matlab, Fortran,<br>C, Python) to:<br>a) Compute the Global Stiffness Matrix of the problem<br>b) Compute the Reduced Stiffness Matrix of the problem<br>c) Solve for the unknown displacements<br>d) Solve for unknown reactions<br>

Extracted text: Assuming to have an input file describing a generic assemblage of beams in, e.g., the following form: Element number I Node i I Node j Elem. Area I Elem Inertia IEILIO 1 1 A1 E1 L1 01 2 1 A2 12 E2 L2 02 3 3 4 АЗ 13 E3 L3 ӨЗ N k AN IN EN LN ON and Node num I Nodal Displ u I Nodal Displ v I Nodal rot O | BC Fx | BC Fy | BC M | 1 1 1 F1y 1 2 1 1 F2x 1 M2 3 1 1 M3 N 1 1 1 FNx FNy MN * 1-> unknown write a code in your preferred computer language or environment (e.g. Matlab, Fortran, C, Python) to: a) Compute the Global Stiffness Matrix of the problem b) Compute the Reduced Stiffness Matrix of the problem c) Solve for the unknown displacements d) Solve for unknown reactions

Jun 08, 2022
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