Weight Lifter Analogy
Consider the weight lifter given below. In first case he is able to lift maximum up to 50 k.g in a relatively simple fashion. Now consider the second case, is it true to say here also his maximum lifting ability is 50 k.g?. Answer to this question could be Yes or No. But if you can well assume his lifting ability is same in second case also , then this can be considered as failure theory for a weight lifter.Backbone of Failure Theories
In materials also we can apply the same concept of weight lifter failure theory.Here material will undergo a simple force test(simple tension test), so one can determine what's the maximum load capability material has got. Now we will assume that in a complex loading condition also material has same capability. This assumption forms backbone of Failure theories.Concepts of Simple tension test and Principal stresses are main 2 prerequisites to understand Failure theories effectively.Simple Tension Test
In Simple tension test material is pulled from both the ends,elongation of material(strain) with respect to load is noted. From such an observation one can easily determine maximum strength of the material. For ductile material upper yield point is considered to be maximum strength of material, while for brittle material it is taken as ultimate strength of the material. From maximum strength value of material values of various other parameters can easily be calculated.Simple tension graph and upper yield point value for a ductile material case is shown in figure below.Fig.1 Simple tension test |
Principal Stress
Principal stress is the maximum normal stress occurring at a given point. In order to find out this value easy way is to do Mohr circle analysis. Once you know Principal stress values you can go ahead with failure theories.Figure below shows principal stress values induced at point in 3 dimensional complex loading case.Fig.2 Principal stresses and planes |
Failure Theories
Just by looking name of the theory you will be able to formulate condition of failure in an actual case, if your concept of STT and Principal stresses are clear. The theories along with its usability is given below.- Maximum principal stress theory - Good for brittle materials* According to this theory when maximum principal stress induced in a material under complex load condition exceeds maximum normal strength in a simple tension test the material fails. So the failure condition can be expressed as
- Maximum shear stress theory - Good for ductile materials According to this theory when maximum shear strength in actual case exceeds maximum allowable shear stress in simple tension test the material case. Maximum shear stress in actual case in represented as
- Maximum normal strain theory - Not recommended This theory states that when maximum normal strain in actual case is more than maximum normal strain occurred in simple tension test case the material fails. Maximum normal strain in actual case is given by
- Total strain energy theory - Good for ductile material According to this theory when total strain energy in actual case exceeds total strain energy in simple tension test at the time of failure the material fails. Total strain energy in actual case is given by Total strain energy in simple tension test at time of failure is given by So failure condition can be simplified as
- Shear strain energy theory - Highly recommended According to this theory when shear strain energy in actual case exceeds shear strain energy in simple tension test at the time of failure the material fails. Shear strain energy in actual case is given by
Maximum shear stress in simple tension case occurs at angle 45 with load, so maximum shear strength in a simple tension case can be represented as Comparing these 2 quantities one can write the failure condition as
Maximum strain in simple tension test case is given by So condition of failure according to this theory is Where E is Youngs modulus of the material
Shear strain energy in simple tension test at the time of failure is given by So the failure condition can be deduced as Where G is shear modulus of the material