Thermal Expansion Stress

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SUMMARY

The discussion focuses on designing a system for thermally cycling a stainless steel substrate up to 1200°C while preventing buckling during thermal expansion. The substrate dimensions are 4"x1"x1/16", and the selected bolts are Monel with a nominal diameter of 3mm. The critical compressive stress calculated for the substrate is 22.9 ksi. The main challenge is incorporating the thermal expansion of both the substrate and the bolts to determine the compressive stress on the sample accurately.

PREREQUISITES
  • Understanding of thermal expansion coefficients for materials
  • Knowledge of compressive stress calculations
  • Familiarity with material properties of stainless steel and Monel
  • Experience with superposition principles in thermal stress analysis
NEXT STEPS
  • Research methods for calculating thermal expansion in composite materials
  • Learn about the superposition method for thermal stress analysis
  • Investigate the mechanical properties of Monel and its behavior under thermal cycling
  • Study buckling analysis techniques for thin-walled structures
USEFUL FOR

Mechanical engineers, materials scientists, and designers involved in high-temperature applications and thermal stress analysis will benefit from this discussion.

Seraph042
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I'm designing a system that will thermally cycle a stainless steel substrate up to 1200C from room temperature; right now my design consists of clamping the substrate onto a plate using a bolt head/washer with a nut on the other end of the screw, as shown on the attached figure.

I want to determine the minimum distance I can put the substrate away from the bolt so that buckling will not occur during thermal expansion. The substrate in question is 4"x1"x1/16" (the 1" is into the figure). The bolts I have selected have a 3mm nominal diameter and are made of Monel.

I calculated the critical compressive stress on the substrate to be 22.9 ksi, but I am having trouble incorporating the thermal expansion of both the sample and the bolt in order to determine the compressive stress on the sample. What steps should I take?

Here's some material info I got from matweb.com:

\alpha_{stainless steel}=15.1E-06 /degC, E_{stainless steel}=28.5E+06 psi, S_{y, stainless steel}=89.6E+03 psi

\alpha_{bolt}=13.9E-06 /degC, E_{bolt}=24.5E+06 psi
 

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When looking at thermal stresses, the typical approach is superposition. Assume that you have a beam fixed between two supports and heat it. You can think of there being two loads: one thermal, and one mechanically imposed by the support.

Typically one would allow a free end to move as if it were not being constrained. You would then calculate the load required to move it back into place.

I hope that gets you on the right track. If you need an example I'm sure someone can provide one.
 

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