In essence, strain transformation is pretty much the same as stress transformation; except that σx and σy are swapped with εx and εy. *However τxy is actually converted to γxy/2 instead (you can check any textbooks for the derivation to see why).
Again, the equations are presented for completeness sake and it’s still recommended for you to use the Mohr’s circle instead, which we will cover in Chapter 8.2.
In essence, strain transformation is pretty much the same as stress transformation; except that σx and σy are swapped with εx and εy. *However τxy is actually converted to γxy/2 instead (you can check any textbooks for the derivation to see why).
Again, the equations are presented for completeness sake and it’s still recommended for you to use the Mohr’s circle instead, which we will cover in Chapter 8.2.
And here are the formulas for principal strains ε1, ε2 and the maximum in-plane shear strain γmax in-plane:
*Always, always remember to multiply γx'y'/2 by 2 after conversion to get the final γx'y'. Students always miss this crucial last step as they get carried away after performing the long transformations.
Let’s look at an example now.
And here are the formulas for principal strains ε1, ε2 and the maximum in-plane shear strain γmax in-plane:
*Always, always remember to multiply γx'y'/2 by 2 after conversion to get the final γx'y'. Students always miss this crucial last step as they get carried away after performing the long transformations.
Let’s look at an example now.