Exercises in continuum mechanics

AI Thread Summary
The discussion focuses on solving exercises in continuum mechanics involving stress tensors and plain stress conditions. The first exercise requires calculating the stress component σx to ensure a stress vector face is nil at the origin, while also determining the normal vector components. The second exercise involves deriving expressions for σx and σy at point M(1,1) given a shear stress of 1/2, leading to results σx = a + 3b and σy = 4a + 2b. The participant confirms the use of the Airy function in their calculations and resolves the equations related to the stress tensor. The thread concludes with the participant expressing satisfaction in finding the answers to the posed problems.
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Hello
Please forgive me if i am not posting in the correct forum. Also you may find my English a bit rusty since i am basically French

Ok so i want to solve some exercises in continuum mechanics . The first exercise states :
we have a stress tensor in a Cartesian coordinate system with the point O ; origin of the system , such as :
captur10.jpg

calculate σx so that one face of the stress vector is nil at point 0 ( i know it sounds odd)
Then , calculate the components of the vector n on this face .

Another exercise states : the function of a stress for a plain stress condition is given by :
captur11.jpg

Where a and b are constants and the volume forces are ignored .
Determine the expressions of σx and σy if for the point M(1,1) the shear stress is equal to 1/2.

For the last exercise , what i have done is calculate the derivative of Φ with respect to x and did that again for y , then calculate the the two derivative functions for the point M so it gave me :
σ1 =a+3b
σ2=4a+2b
after that i applied the know functions to calculate σx and σy for a plain stress problem
it gave me these results :
σx =a+3b
σy= 4a+2b which equal exactly my first results ( not sure if this is correct tho )
Thanks
 
Last edited:
yea well i found out the responses to the question . for the first one , you just need to resolve the serie of nul equations ( the stress tensor multiplied by the n vecteur equal 0)
for the last problem , that function is called the Airy function .
 
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