Chapter 4, Problem 4.44P

Interpretation Introduction

Interpretation:

The slip systems made up of close-packed planes and the directions activated because of the applied stress needs to be determined.

Concept Introduction:

The expression for the Schmidt s law is as follows:

  ${\tau }_r=\sigma \cos \lambda \cos \varphi \mathrm{........}\left(1\right)$

Here, ${\tau }_r$ is the resolved shear stress, $\sigma$ is the applied stress, $\lambda$ is the angle between the slip direction and the applied force, and $Ø$ is the angle between the normal to the slip plane and the applied force.