Analytical solution for bending stiffness of tapered tube

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Discussion Overview

The discussion focuses on deriving the formula for the bending stiffness of an isotropic tapered tube that is cantilevered with a point load applied at the free end. Participants explore theoretical approaches, mathematical formulations, and the challenges associated with finding an analytical solution.

Discussion Character

  • Exploratory
  • Technical explanation
  • Mathematical reasoning

Main Points Raised

  • One participant inquires about deriving a formula for bending stiffness using the Euler-Bernoulli beam equation.
  • Another participant expresses uncertainty about the existence of an analytical formula and suggests starting from first principles, detailing the relationship between deflection, bending moment, modulus of elasticity, and the second moment of area.
  • A participant reiterates the previous points and emphasizes the need for a common formula to find bending stiffness at various distances along the tube.
  • One participant provides specific expressions for the external and internal radii of the tube as functions of distance from the fixed end, along with the formula for the second moment of area.
  • The bending stiffness is defined as the product of the modulus of elasticity and the second moment of area, although it is noted that substituting the radius expressions into the moment of area formula may involve complex algebra.

Areas of Agreement / Disagreement

Participants do not reach a consensus on the existence of an analytical formula for bending stiffness, with some expressing doubt about its feasibility while others propose methods to derive it.

Contextual Notes

Participants acknowledge that the integration of the moment equation may not yield an analytical solution and suggest that numerical methods might be more practical. The discussion also highlights the complexity of algebra involved in deriving the second moment of area from the radius expressions.

Sud89
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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?
 
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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.
 
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.
upload_2014-11-22_2-29-23.png

This is the model of the tube that I have. I need to derive a common formula in order to find the bending stiffness at different distances. say x=1,2,3..
 
At x = 0, let the external radius of the tube be RO and the internal radius be RI

For the values of RO and RI at a distance x from the fixed end then,

RO(x) = RO - x * tan α
RI (x) = RI - x * tan α

The second moment of area of the tube is then

I(x) = (π/4)*[RO(x)4 - RI(x)4]

and the bending stiffness = E I(x)

If you want to substitute the first expressions for RO(x) and RI(x) into I(x), well, it's probably a lot of algebra to clean up.
 

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