Calculating the Schmid factor for an FCC single crystal

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SUMMARY

The Schmid factor for an FCC single crystal oriented with its [100] direction parallel to the loading axis is calculated using the formula "cos(φ) * cos(λ)", where φ is the angle between the slip direction and the loading direction, and λ is the angle between the loading direction and the slip direction. The slip planes for FCC crystals are the four {111} planes, with slip directions being the three <110> directions. The correct calculation of the Schmid factor yields a value of 0.408 when using appropriate slip directions within the {111} planes. Incorrect slip direction selection can lead to erroneous results, as demonstrated in the discussion.

PREREQUISITES
  • Understanding of Schmid's Law and resolved shear stress
  • Familiarity with FCC crystal structures and slip systems
  • Knowledge of trigonometric functions and their application in crystallography
  • Ability to perform vector calculations in three-dimensional space
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  • Study the calculation of Schmid factors for different crystal orientations
  • Learn about the mechanics of slip systems in FCC and BCC crystals
  • Explore the implications of slip direction selection on material deformation
  • Investigate the role of crystallographic orientations in material strength
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Materials scientists, mechanical engineers, and students studying crystallography or material deformation mechanics will benefit from this discussion.

jbrown110
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The problem said:
"Determine the magnitude of the Schmid factor for an FCC single crystal oriented with its [100] direction parallel to the loading axis. "

The Schmid factor is the

"cos(\phi)*cos(\lambda)"

term in the equation for resolved shear stress.

I know that the slip planes for an FCC single crystal are the four {111} planes, and the slip directions are the three <110> directions inside each of the {111} planes.

To solve for \phi, the angle between the <111> direction and the loading direction, <100>, I said that it was equal to

Cos^{-1}((1*1+1*0+1*0)/\sqrt{(1^2+1^2+1^2)*(1^2)})

That comes out to 1/\sqrt{3}

And using the same equation, I found that \lambda, the angle between the loading direction, <100>, and the slip direction, <01-1>, is \pi/2

Multiplying \phi and \lambda should have given me the schmid factor, according to my textbook, but I couldn't get the right answer.

The answer is .408, but I kept getting something different and I'm not sure why. If some one could explain this to me, I would be very grateful. Thanks
 
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Hi jbrown110, welcome to PF. Your slip direction doesn't lie within your slip plane. You're going to have a hard time obtaining slip that way. :smile:
 
So, basically I picked the one direction that doesn't work for the [111] plane. haha

I reworked it with the other two possible slip directions and they both gave the right answer.

Thanks for the reply.
 
You're welcome!
 

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