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Q.1. A plane truss is loaded and while solving for internal forces in truss members we are able to formulate the ten equation

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%formulating and solving ten liner eqautions Ax = b
%first create the coefficient matrix A i.e. LHS
%column/variables are in the following order:
%Ax|Ay|Ey|AD|AB|BC|BD|CE|CD|DE => 10 columns
A= [
1, 0, 0, 1, 0, 0, 0, 0, 0, 0;
0, 1, 0, 0, 1, 0, 0, 0, 0, 0;
0, 0, 0, 0, 0, 1, 0.6, 0, 0, 0;
0, 0, 0, 0, -1, 0, -0.8, 0, 0, 0;
0, 0, 0, 0, 0, -1, 0, 0.6, 0, 0;
0, 0, 0, 0, 0, 0, 0, -0.8, -1, 0;
0, 0, 0, -1, 0, 0, -0.6, 0, 0, 1;
0, 0, 0, 0, 0, 0, 0.8, 0, 1, 0;
0, 0, 0, 0, 0, 0, 0, -0.6, 0, -1;
0, 0, 1, 0, 0, 0, 0, 0.8, 0, 0;
]
% b is the RHS of constants
b = [0; 0; -74; 0; 0; 24; 0; 0; 0; 0]
% x is the solution corresoponding to the same order as colums in A
x = inv(A)*b
x

SCREENSHOTS

trusslinearSolve.m* ×1+ %formulating and solving ten liner eqaut ions Ax = b first create the coefficient matrix A i.e. LHS %

OUTPUT

Command Window >>trusslinearSolve 1.0000 0 1.0000 0 1.0000 0 0 -1.0000 0 0 1.0000 0 0.6000 0 -0.8000 0 0 0 1.0000 0 -1.0000 0-74.0000 -37.3333 61.3333 74.0000 37.3333 -46.0000 46.6667 76.6667 37.3333 46.0000

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Q.1. A plane truss is loaded and while solving for internal forces in truss members we are able to formulate the ten equations given below: Ax +AD0; Ay +AB074+ BC+H(3/5) BD 0 BC +(3/5) CE-0 CD + (...
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