Prandtl stress function for circular bar in torsion

In summary, for a Prandtl stress function to be valid, it must be zero on the boundary. Both functions provided, ##\phi_1## and ##\phi_2##, satisfy this condition for a circular bar. However, when calculating the internal torque M using these functions, the solutions diverge. This discrepancy can be explained by the fact that the units for ##C## in both functions are different, resulting in different values. By setting ##C_{\phi_2} = \frac{C_{\phi_1}}{r^2}##, we can verify that the two functions are indeed equal and thus have the same solution for internal torque. This discrepancy can also be resolved by checking the deriv
  • #1
davidwinth
103
8
TL;DR Summary
When applying two different (but equivalent) stress functions for a circular bar, two different results appear.
For a Prandtl stress function to be valid, it must be zero on the boundary. For a circular bar, both of these work:

$$\phi_1 = C\left(\frac{x^2}{r^2}+ \frac{y^2}{r^2} - 1\right)$$

$$\phi_2 = C \left(x^2+ y^2- r^2\right)$$

But performing the integration for the internal torque M gives divergent solutions. Since both functions are legitimate, which one is the "correct" one and why doesn't the other one work?

$$M = 2 \int \int_A \phi_1dxdy = -C \pi r^2$$

$$M = 2 \int \int_A \phi_2 dxdy = -C \pi r^4$$
 
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  • #2
Have you checked the derivations in Timoshenko's "Theory of Elasticity" ? There you may find the answer to your question.
 
  • #3
Obviously, the units of ##C## in both ##\phi_1## and ##\phi_2## are different, thus they probably have different values as well.

Since ##r## is a constant, my guess is that ##C_{\phi_2} = \frac{C_{\phi_1}}{r^2}##.

$$\phi_1 = C_{\phi_1}\left(\frac{x^2}{r^2}+ \frac{y^2}{r^2} - 1\right) = \frac{C_{\phi_1}}{r^2}\left(x^2+y^2 - r^2\right) = C_{\phi_2}\left(x^2+y^2 - r^2\right) = \phi_2$$

Therefore we can verify this equality:
$$M_{\phi_1} = M_{\phi_2}$$
$$-C_{\phi_1} \pi r^2 = -C_{\phi_2} \pi r^4$$
$$-C_{\phi_1} \pi r^2 = -\frac{C_{\phi_1}}{r^2}\pi r^4$$
$$-C_{\phi_1} \pi r^2 = -C_{\phi_1}\pi r^2$$
 

FAQ: Prandtl stress function for circular bar in torsion

What is the Prandtl stress function for a circular bar in torsion?

The Prandtl stress function is a mathematical function used in solid mechanics to describe the stresses and displacements in a circular bar under torsional loading. It is a solution to the governing equations of elasticity and can be used to determine the stress and displacement fields in the bar.

How is the Prandtl stress function derived?

The Prandtl stress function is derived by assuming a particular form for the displacement field in the circular bar and then using the equations of equilibrium and compatibility to solve for the stress components. The final form of the stress function is determined by satisfying the boundary conditions of the problem.

What are the advantages of using the Prandtl stress function method?

The Prandtl stress function method allows for a simplified solution to the problem of a circular bar in torsion. It reduces the number of unknowns and equations that need to be solved compared to other methods, making it more efficient and easier to use. It also provides insight into the stress and displacement fields, which can be useful for engineering design and analysis.

Can the Prandtl stress function be used for non-circular bars?

No, the Prandtl stress function method is only applicable to circular bars. This is because it relies on the assumption of axisymmetric loading and displacement fields, which is only true for circular geometries. For non-circular bars, other methods such as the Saint-Venant torsion theory must be used.

Are there any limitations to using the Prandtl stress function method?

One limitation of the Prandtl stress function method is that it assumes the material of the bar is isotropic, meaning it has the same mechanical properties in all directions. This may not be the case for some materials, and in those situations, the method may not accurately predict the stress and displacement fields. Additionally, the method is only valid for small deformations and does not account for large displacements or yielding of the material.

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