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Which theory of failure will you use for aluminium components under steady loading is    

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Which theory of failure will you use for aluminium components under steady loading is                                                        

      (a) principal stress theory

      (b) principal strain theory

      (c) strain energy theory

      (d) maximum shear stress theory
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what is the answer?

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answered by (140 points)
pls email me the answer with reason i have been searching for this answer , rvpran@gmail.com

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