Thursday, 12 May 2022

Structural Analysis of Plane Truss using Scilab

 

Input data

F  = 

   0.
   0.
   0.
  -50.
   0.
  -50.
   0.
   0.
   0.
   0.
External force vector

U  = 

   0.
   0.
   0.0017857
  -0.0108753
  -0.0017857
  -0.0108753
   0.
   0.
   0.
  -0.0117682
Deflection vector output

F=
  -55.901699
25
  0
  -25
0
25
  -55.901699

Member forces

ans  =

   1.   25.   50.

 ans  =

   4.  -25.   50.
Support reaction


Truss original and deflected shape


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