Problem on stiffness matrix of beam and deflection of tapered beam

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SUMMARY

The discussion focuses on deriving the stiffness matrix for a beam with nodal linkage and calculating the deflection of a tapered beam. The first participant suggests setting the first row of the stiffness matrix to zero due to the shear force at the first node being zero. For deflection, the second participant proposes using the relationship between EI and the moment equation, specifically integrating the equation d²y/dx² = -M/EI, where I is a function of x. The integration must incorporate boundary conditions based on the specific setup of the tapered beam.

PREREQUISITES
  • Understanding of beam theory and stiffness matrix formulation
  • Knowledge of moment-curvature relationships in structural analysis
  • Familiarity with differential equations and integration techniques
  • Experience with tapered beam properties and inertia functions
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  • Study the derivation of stiffness matrices for beams with nodal linkages
  • Learn about the integration of differential equations in structural mechanics
  • Explore the effects of varying inertia on the deflection of tapered beams
  • Review boundary condition applications in beam deflection problems
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Structural engineers, mechanical engineers, and students studying beam mechanics who are involved in analyzing stiffness matrices and deflection in tapered beams.

chiraganand
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1.How do i derive the stiffness matrix for a beam with nodal linkage? ie the shear force at the first node is 0 but the usual shear and moment resistance is present for the second node.

I thouth about solving the problem by just putting the first row of the stiffness matrix as 0 . Am i correct? Plee help in this

2. How do i get the deflection of a tapered beam? i have the intertia as a function of x. How do i go about the problem?
I thought of using the the the relation between EI and Moment equation and integrating it. But i a m not sure how to go further. Can someone please help me in this
 
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chiraganand said:
2. How do i get the deflection of a tapered beam? i have the intertia as a function of x. How do i go about the problem?
I thought of using the the the relation between EI and Moment equation and integrating it. But i a m not sure how to go further. Can someone please help me in this

Your moment equation would be

EI (d2y/dx2) = -M

where I is a function of x.

So you'd need to just do

d2y/dx2 = -M/EI

then integrate twice inputting your boundary conditions. This would depend on how your tapered beam is set up.
 
1. I am having trouble visualizing your beam and the nature of this 'nodal linkage'. Can you provide a picture?
 

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