Mechanics Of Materials & Structures Online Test - Paper 3
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Mechanics of Materials & Structures Online Test – Paper 3

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Created by 83a36dcfd5c4caff12bc80f0020c9c749e12cbbbdb7c406dc1dd39996cb85836?s=32&d=monsterid&r=g gkaimVikash chaudhary

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  • Total Questions: 50
  • Time Allotted: 50 minutes
  • Passing Score: 70%
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1. How does Young's Modulus vary with an increase in temperature?

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2. The variation of the bending moment in the segment of a beam where no external load is present is

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3. *The forces which meet at one point, but their lines of action do not lie in a plane, are called:

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4. *The compression test is commonly used for testing

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5. Along the neutral axis of a simply supported beam

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6. The difference in ordinate of the shear force between any two sections is equal to the area under

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7. "When a rectangular beam is loaded transversely the maximum compressive stress is developed on the :

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8. *The rate of change of shear force is called

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9. *Proof resilience is the greatest stored energy at

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10. A Prismatic bar when subjected to pure bending assumes the shape of

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11. Which of the following is a relatively ductile material?

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12. *Which of the following sections is the most efficient in carrying bending moments

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13. *In the case of a fixed beam loaded at a point at its center, the number of points at which BM is zero

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14. *Stress may be defined as force

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15. If the Poisson's ratio of a material is 0.25, the ratio of Modulus of Rigidity to the Young's Modulus is

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16. The expression EI(d^4y/dx^4) at any section for a beam is equal to

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17. *Mathematically, strain may be defined as

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18. *The total time of collision and restitution of two bodies is called

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19. In the case of an H section, the maximum shear stress will occur at

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20. A viscoelastic material

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21. *A member with a cross section of a mm^2 is subjected to a force of P N. It is L mm long and of Young's Modulus, E N/mm^2. The strain will be

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22. A cantilever beam of span 4m and carrying a point load of 10 kN located at 3m from the fixed end. Find the BM at the fixed and free end

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23. A column that fails primarily due to direct stress is called

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24. The effective length of a column effectively held in position and restrained in direction at one end will be

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25. *Load required to produce unit deflection is called

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26. In rectangular column having cross section b X h, the core is

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27. Normally, the numerical value of Poisson's is

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28. A beam fixed at both ends with a central load W in the middle will have zero bending moment

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29. The square root of the ratio of moment of inertia and cross-section area of the member is known as

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30. *The velocity of a moving body is:

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31. *Hooke's law holds good up to:

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32. *The centre of gravity of a triangle is at the point where three

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33. The diagram showing the variation of BM along the span of the beam is called

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34. *The relation between the radius of curvature (R), bending moment (M), and flexural rigidity (EI) is given by

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35. *The ratio of change in volume to the original volume is called:

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36. The section modulus of a circular section about an axis through its C.G. is

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37. *A beam is said to be of uniform strength if

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38. *The slope of an elastic curve at the point of contraflexture

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39. *The shear force and bending moment are related by

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40. *Compression members always tend to buckle in the direction of the

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41. A long vertical member subjected to an axial compressive load is called

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42. *"A simply supported beam of span L carries a uniformly distributed load W. The maximum bending moment, M is:

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43. Shear strain is defined as

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44. Permanent set is

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45. The shear center may be defined as

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46. *Strut is a

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47. The moment of inertia of a triangular section b x h about the base is

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48. *In a simply supported beam with span (L) having a triangular load with its intensity 0 at both ends and W at center. The maximum BM will be

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49. Identify the correct relationship that exists among the modulus of elasticity (E), modulus of rigidity (N), and bulk modulus (k) is

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50. Shape of the bending moment diagram for a simply supported beam having a point load at the center is

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