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1. The maximum normal stress theory is used for





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MCQ->Consider the following statements : 1. In a member subjected to uniaxial tensile force the maximum normal stress is the external load divided by the maximum cross-sectional area. 2. When the structural member is subjected to uniaxial loading, the shear stress is zero on a plane where the normal stress is maximum. 3. In a member subjected to uniaxial loading, the normal stress on the planes of maximum shear stress is less than the maximum. Of these statements :....
MCQ->Consider the following statements : In a uni-dimensional stress system, the principal plane is defined as one on which the 1. shear stress is zero. 2. normal stress is zero. 3. shear stress is maximum. 4. normal stress is maximum. Of these statements :....
MCQ->The design stress, which is more than the damaging stress, is the least unit stress that will render a member unfit for service before the end of its normal life. The design stress factor or factor of safety indicates the margin between design stress and the __________ stress.....
MCQ->A shaft is subjected to a maximum bending stress of 80 N/mm2 and maximum shearing stress equal to 30 N/mm2 at a particular section. If the yield point in tension of the material is 280 N/mm2 and the maximum shear stress theory of failure is used, then the factor of safety obtained will be....
MCQ->A body is subjected to a tensile stress of 1200 MPa on one plane and another tensile stress of 600 MPa on a plane at right angles to the former. It is also subjected to a shear stress of 400 MPa on the same planes. The maximum normal stress will be....
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