Truss Bridge Tension and Compressions

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SUMMARY

The discussion focuses on calculating tension and compression forces in a truss bridge subjected to a CL-625 design truck load of 625 kN. The span of the bridge is 50 meters, divided into 8 sections, with specific dimensions and angles. The correct approach involves using the equations for bending moment (M = PL/4) and tension (T = M/H), while also applying the Method of Joints or Sections to determine forces in all members. The initial calculations provided were deemed insufficient as they did not account for forces in diagonal and vertical members.

PREREQUISITES
  • Understanding of truss bridge design principles
  • Familiarity with the Method of Joints and Method of Sections
  • Knowledge of bending moment calculations
  • Proficiency in stress analysis, specifically tensile and compressive stresses
NEXT STEPS
  • Study the Method of Joints for analyzing truss forces
  • Learn about the Method of Sections for determining internal forces in trusses
  • Explore the calculation of areas for structural members using T = phi*As*Fy
  • Review the principles of bending moment and shear force in structural analysis
USEFUL FOR

Civil engineers, structural analysts, and students studying truss bridge design and analysis will benefit from this discussion.

noahsc
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Homework Statement


Given the weight of a CL-625 design truck (625 kN) on a truss bridge of span 50m, divided into 8 sections (each 6.25 m) with a height of 6.25m making 45deg angles and a width of 6m, what are the tension and compression forces of the members?
pratt-1.jpg



Homework Equations



Mb = PL/4
T=M/H

The Attempt at a Solution


Using these equations, I got a total tension of 625kN.. I don't know if I'm using the equations wrong or I'm missing something completely, but that seems like a very small number.
 
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You are not using correct equations...Trusses are subjected primarily to tensile and compressive stresses in each member from member forces under the applied loads, whereas Beams are subject to bending stresses from bending moments under the applied loading. Two different processes. You need to find the force in each member...where is the load placed?
 
yeah I am going to restate the title.
this is only part of the problem. what i need to find is the area of the lower and upper chords with the equation T = phi*As*Fy with the Fy=350Mpa

So, what I have been instructed on doing is find the bending moment of the live load M=PL/4 and then find the tension using the moment arm of the height (or vertical truss)
 
noahsc said:
yeah I am going to restate the title.
this is only part of the problem. what i need to find is the area of the lower and upper chords with the equation T = phi*As*Fy with the Fy=350Mpa

So, what I have been instructed on doing is find the bending moment of the live load M=PL/4 and then find the tension using the moment arm of the height (or vertical truss)
Your answer for the top chord max force of 625 kN compression, and bottom chord max force of 625 kN tension appears correct, but generally, this is not the way to proceed. There are forces in the diagonal and vertical members also,,,,,forces in all members should be found using the trusss Method of Joints or Sections.
 

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