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How to derive the formula to find the bending stiffness of an isotropic tapered tube which is cantilevered with a point load applied at the free end?
The discussion focuses on deriving the analytical formula for the bending stiffness of an isotropic tapered tube cantilevered with a point load at the free end. The Euler-Bernoulli beam equation is central to this analysis, where the bending moment M(x) is defined as -E I(x) d²w(x)/dx². The second moment of area I(x) is calculated using the external radius RO and internal radius RI, both expressed as functions of the distance x from the fixed end. While an analytical solution may be complex, numerical methods are suggested as a practical alternative.
PREREQUISITESMechanical engineers, structural analysts, and students studying beam theory and structural mechanics will benefit from this discussion.
SteamKing said:I'm not sure that there is an analytical formula.
You can always go back to first principles and the Euler-Bernoulli beam equation.
If w(x) = the deflection of the beam at a distance x from the fixed end, then
M(x) = -E I(x) d2w(x)/dx2
where M(x) is the bending moment,
E is the modulus of elasticity, and
I(x) is the second moment of area of the beam cross section at a distance x from the fixed end
For this beam, at the fixed end both the slope and deflection will be zero.
If you can write I(x) as a function of x, you might be able to integrate the moment equation twice and apply the initial conditions to determine the constants of integration. There's no guarantee that the resulting integral can be determined analytically, although a numerical solution would probably be more practical.