Problem on stiffness matrix of beam and deflection of tapered beam

AI Thread Summary
To derive the stiffness matrix for a beam with nodal linkage, it is suggested that the first row can be set to zero due to the absence of shear force at that node. For calculating the deflection of a tapered beam with varying inertia, the relationship between EI and the moment equation is crucial. The moment equation can be expressed as EI (d²y/dx²) = -M, where I is a function of x. Integrating this equation twice while applying appropriate boundary conditions will yield the deflection, but visualization of the beam's configuration is necessary for clarity. Providing a diagram of the beam setup may help in further understanding the problem.
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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