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. Which one is correct if the deflection of a beam is y

2 / 50

2. Centrifugal force acts away from the center of the path while centripetal force

3 / 50

3. Moment of inertia of a rectangular beam bxd is

4 / 50

4. A column that fails primarily due to buckling is known as

5 / 50

5. *"If a rod is simultaneously pulled at both of its ends, it will be a case of:

6 / 50

6. *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

7 / 50

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

8 / 50

8. The method of increasing fatigue resistance by overstressing the metal by successively increasing the loading is known as

9 / 50

9. Maximum bending moment occurs at the center if the simply supported beam is subjected to

10 / 50

10. The moment of inertia of a square section is given by

11 / 50

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

12 / 50

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

13 / 50

13. *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

14 / 50

14. *A point where SF is zero, BM is

15 / 50

15. An orthotropic material has

16 / 50

16. *The ratio of the intensity of stress in a case of a suddenly loaded to that of gradually applied load is

17 / 50

17. The maximum deflection in a cantilever beam carrying a uniformly distributed load (w) over spans is (Where L is span of beam, W is total load and EI is flexural rigidity)

18 / 50

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

19 / 50

19. At the point of application of concentrated load on a beam, there is

20 / 50

20. *Dead load of a member is the

21 / 50

21. Point of contraflexure is a point where bending moment

22 / 50

22. The algebraic sum of the shear flow of a section in any direction must be equal to

23 / 50

23. The moment of inertia of an area will be least with respect to

24 / 50

24. *The shear flow in a section can be defined as

25 / 50

25. *The simple bending equation is

26 / 50

26. For keeping the stress wholly permissible, the load may be applied to a circular column anywhere within a concentric circle of diameter

27 / 50

27. *Bending moment diagram of a simply supported beam having a uniformly distributed load is

28 / 50

28. An isotropic material has

29 / 50

29. The shear center in the case of a T-beam section is

30 / 50

30. *The stress at which the extension of a material takes place more quickly as compared to the increase in load is called

31 / 50

31. Which of the following materials will have the highest Young's Modulus?

32 / 50

32. How does Young's Modulus vary with an increase in temperature?

33 / 50

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

34 / 50

34. The bending moment diagram for a cantilever beam subjected to a moment at the end of the beam would be

35 / 50

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

36 / 50

36. Find the value of thrust, if the member (beam) is subjected to an inclined force having a magnitude of 5 kN and an inclination with the vertical of 30°

37 / 50

37. *In a simply supported beam subjected to a point load at the center, the maximum bending moment occurs at

38 / 50

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

39 / 50

39. The maximum bending moment caused on a simply supported beam subjected to two equal concentrated loads (W/2) spaced at an equal distance (L/3) over the span is

40 / 50

40. In an I section, almost all the shear force is taken by

41 / 50

41. The impact tests are used to determine

42 / 50

42. Rate of change of bending moment is equal to

43 / 50

43. The difference between BM values at any two sections will be equal to

44 / 50

44. The bending moment in a cable carrying a system of loads will be

45 / 50

45. The maximum number of transverse shear forces possible at one end of an element of a plane frame are

46 / 50

46. The region of c/s of a column in which compressive load may be applied without producing tensile load is known as

47 / 50

47. If a material has identical properties in all directions, it is said to be

48 / 50

48. The variation of the bending moment in the portion of the beam carrying a linearly varying load is

49 / 50

49. The difference between SF values at any two sections will be equal to

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

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