Truss stress compressive/tensile stress

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SUMMARY

The discussion focuses on determining the appropriate metal for truss members based on their stress types, specifically compressive and tensile stress. The user confirms the use of the tensile stress formula (Sigma = Force/Area) and seeks clarification on the compressive stress calculation. It is established that compressive truss members should be treated as columns, requiring the calculation of the critical buckling load using the formula Pcr = (pi/L)^2 E I, where Pcr is the critical buckling force, L is the length of the column, E is the modulus of elasticity, and I is the minimum area moment of inertia.

PREREQUISITES
  • Understanding of tensile stress calculations (Sigma = Force/Area)
  • Knowledge of compressive stress and buckling concepts
  • Familiarity with the modulus of elasticity (E) and moment of inertia (I)
  • Basic principles of structural engineering and truss design
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  • Study the critical buckling load calculations for various materials
  • Learn about the properties of different metals used in truss construction
  • Research the implications of slenderness ratios in column design
  • Explore advanced structural analysis techniques for truss systems
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Structural engineers, mechanical engineers, and students involved in truss design and analysis, particularly those focusing on material selection and stress calculations.

peet_dk
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Hi

I have found out which truss member that have compressive stress, and which have tensile.
Now I have to select the metal for each member, I know how to find it when it is simple tensile stress (Sigma=Force/Area) But I think there is another equation when it is compressive stress, or?

Do I have to calculate the compressive truss member as a column, and find the critical buckling load?
 
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Yes. The buckling equation for long slender members is Pcr = (pi/L)^2 E I, where Pcr is the critical buckling force, L is the length of the column, E is the modulus of elasticity of the material you're using, and I is the minimum area moment of inertia (second moment of area) for the cross-sectional shape you're using.

-David
 

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