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Shareware:  MSO.exe  (C++ matrix object-oriented structural analysis).  Shareware description is here.    Download MSO.zip here.

1. Simple 2D square truss with diagonal cross brace

Screen shot:  External loads, internal bar forces and fixed node reactions.  Bars in tension (blue).  Bars in compression (red).

 

2.  Complex 3D steel triangular section trussed tower loaded at top node

Screen shot:  External loads and internal bar forces.  Bars in tension (blue).  Bars in compression (red).

 

Screen shot:  Static Analysis Sample Output

Nodes in GLOBAL Coordinate Reference Frame:

#              ID             x              y              z              dx            dy            dz            angx        angy        angz

_______________________________________________________________________________________

15            U                0.0         320.0         0.0         7.6e-01   -7.4e-03  0.0e+00  0.0e+00  0.0e+00  0.0e+00

_______________________________________________________________________________________

14            X               10.0        280.0         0.0         6.2e-01   -4.1e-02  0.0e+00  0.0e+00  0.0e+00  0.0e+00

_______________________________________________________________________________________

 

Screen shot:  Static Analysis Sample Output

Member Internal Loads in LOCAL Coordinate Reference Frame:

ID             Node        Euler/Yld                  Fx            Fy            Fz                            Mx           My           Mz

_______________________________________________________________________________________

1              Q             -4.4e+04                  4.7e+03  7.0e+01  0.0e+00                    0.0e+00  0.0e+00  1.8e+03

1              A              3.6e+04                  -4.7e+03  -7.0e+01  0.0e+00                  0.0e+00  0.0e+00  1.1e+03

_______________________________________________________________________________________

2              K              -4.4e+04                  -6.5e+03  7.2e+01  0.0e+00                  0.0e+00  0.0e+00  1.8e+03

2              H               3.6e+04                  6.5e+03  -7.2e+01  0.0e+00                  0.0e+00  0.0e+00  1.2e+03

_______________________________________________________________________________________

3              Q             -3.6e+04                  -4.5e+01  -8.2e+01  0.0e+00                  0.0e+00  0.0e+00  -8.2e+02

3              K               3.6e+04                  4.5e+01  8.2e+01  0.0e+00                    0.0e+00  0.0e+00  -8.3e+02

_______________________________________________________________________________________

 

Screen shot:  Dynamic  Analysis Sample Output

Forming Global Mass Matrix

Forming Global Dynamical Matrix

Determining Fundamental Frequency

Fundamental Frequency = 0.0893 Hz

Fundamental Frequency Period = 11.2 sec

Iterations: 4

Time taken = 2 sec

 

Screen shot:  Input Data

Member Specifications:

ID             Node        Node        A             Imax         Imin          J              W             L              Description

__________________________________________________________________________________________

1              Q             A              1.2e+00  6.8e-01   2.8e-01   1.7e-02   1.4e+01  4.1e+01  ANGLE 2.5 X 2.5 X 1/4

2              K              H               1.2e+00  6.8e-01   2.8e-01   1.7e-02   1.4e+01  4.1e+01  ANGLE 2.5 X 2.5 X 1/4

3              Q             K               1.2e+00  6.8e-01   2.8e-01   1.7e-02   6.7e+00  2.0e+01  ANGLE 2.5 X 2.5 X 1/4

4              K              A              3.1e-01   7.5e-03   7.5e-03   1.5e-02   4.3e+00  5.0e+01  ROUND BAR 5/8      

5              Q             H               3.1e-01   7.5e-03   7.5e-03   1.5e-02   4.3e+00  5.0e+01  ROUND BAR 5/8      

6              Q             I                1.2e+00  6.8e-01   2.8e-01   1.7e-02   1.3e+01  4.0e+01  ANGLE 2.5 X 2.5 X 1/4

 

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Updated: 11/13/2008