Shear Forces and Bending Moments in Beams

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SUMMARY

The discussion focuses on calculating shear forces and bending moments for a 4m beam supported by a hinge and a roller, subjected to a non-uniform load defined by w = 25Cos(πx/8) kN/m. The shear force is derived as -200/π Sin(πx/8) and the bending moment as -400/π² Cos(πx/8). The importance of boundary conditions in determining constant terms in these equations is emphasized, leading to a complete solution for the problem.

PREREQUISITES
  • Understanding of beam mechanics and support types (hinge and roller).
  • Knowledge of integration techniques in calculus.
  • Familiarity with shear force and bending moment diagrams.
  • Concept of boundary conditions in structural analysis.
NEXT STEPS
  • Study the application of boundary conditions in beam analysis.
  • Learn about shear force and bending moment diagrams for various loading conditions.
  • Explore advanced integration techniques relevant to structural engineering.
  • Investigate the effects of different support types on beam behavior.
USEFUL FOR

Students and professionals in civil engineering, structural analysis, and mechanical engineering who are involved in beam design and analysis under various loading conditions.

mit_hacker
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Homework Statement



(Q) A beam 4m long is supported at the left hand side by a hinge support and on the right by a roller support. It is under a non-uniform load intensity throughout by a load intensity given by:

w = 25Cos(pi x/8)kN/m.

Write equations for the shear force and the bending moments for any section of the beam.

Homework Equations



F= -∫▒w
M=-∫▒F

The Attempt at a Solution



I can easily apply the above formulas and integrate.

The shear force comes to -200/π Sin(πx/8).
Similarly, the Moments come to -400/π^2 Cos(πx/8)

But at the back of the book, there is also the constant term along with the term obtained by the integration.

Can someone please help me to calculate them. How did they come about?
 
Last edited:
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mit_hacker said:

Homework Statement



(Q) A beam 4m long is supported at the left hand side by a hinge support and on the right by a roller support. It is under a non-uniform load intensity throughout by a load intensity given by:

w = 25Cos(pi x/8)kN/m.

Write equations for the shear force and the bending moments for any section of the beam.


Homework Equations



F= -∫▒w
M=-∫▒F


The Attempt at a Solution



I can easily apply the above formulas and integrate.

The shear force comes to -200/π Sin(πx/8).
Similarly, the Moments come to -400/π^2 Cos(πx/8)

But at the back of the book, there is also the constant term along with the term obtained by the integration.

Can someone please help me to calculate them. How did they come about?
You've got to look at the boundary conditions to get the constants. What do you know about the bending moment at each support?
 
Ahhhhhhhhh!

That was so simple?:smile:

I can't believe that I didn't see it! Thanks a lot for your help PhantomJay!
 

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