Mechanics Of Materials & Structures Online Test - Paper 3
GK Aim: A Treasure of MCQs

Mechanics of Materials & Structures Online Test – Paper 3

0%
Created by 83a36dcfd5c4caff12bc80f0020c9c749e12cbbbdb7c406dc1dd39996cb85836?s=32&d=monsterid&r=g gkaimVikash chaudhary

This is a FREE online test. Beware of scammers who ask for money to attend this test.

Get fresh, new questions in each attempt.

  • Total Questions: 50
  • Time Allotted: 50 minutes
  • Passing Score: 70%
  • Randomization: Yes
  • Certificate: Yes
  • Do not refresh the page!
  • 👍 All the best!

1 / 50

1. *Which of the following gives Bulk Modulus?

2 / 50

2. The relation between deflection (y) and bending moment (M) is

3 / 50

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

4 / 50

4. For a column of given material, the Rankine's constant depends on

5 / 50

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

6 / 50

6. If the elasticity of the material is zero then the material is said to be

7 / 50

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

8 / 50

8. *The critical bending moment caused in a fixed end beam loaded with a uniformly distributed load (W = wL) throughout is

9 / 50

9. An isotropic material has

10 / 50

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

11 / 50

11. According to Hook's law, which one is correct?

12 / 50

12. If magnitude and direction of a load does not change with respect to time, this type of load is called

13 / 50

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

14 / 50

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

15 / 50

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

16 / 50

16. *Proof resilience is the greatest stored energy at

17 / 50

17. A beam simply supported at ends is subjected to load. The maximum bending moment is located where

18 / 50

18. *The property of a material by which a body returns to its original shape after removal of the force is called

19 / 50

19. The value of buckling load is ... than the crushing load in the case of a long column

20 / 50

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

21 / 50

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

22 / 50

22. Find the elongation of a bar if c/s area of the bar is A, length 1, applied load p, modulus of elasticity of material is E

23 / 50

23. *Load required to produce unit deflection is called

24 / 50

24. A cantilever beam is one which is:

25 / 50

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

26 / 50

26. The ratio of elongations of a conical bar due to its own weight and that of a prismatic bar of the same length is

27 / 50

27. The stress due to temperature change in a member depends on

28 / 50

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

29 / 50

29. *The simple bending equation is

30 / 50

30. *A member which does not regain its original shape after the load producing deformation is removed, is said to be:

31 / 50

31. Shear strain is defined as

32 / 50

32. Find the maximum SF induced in a cantilever beam subjected to a point load of 10 KN and a length of the beam is 10 m. The load is located at a distance of 3 m from the free end

33 / 50

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

34 / 50

34. *The compression test is commonly used for testing

35 / 50

35. The maximum bending moment caused by a large number of equally spaced identical loads on a simply supported beam is (W = wL)

36 / 50

36. Along the neutral axis of a simply supported beam

37 / 50

37. The ratio of moment of inertia of a square section to that of a circular section for a given depth is given by

38 / 50

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

39 / 50

39. The maximum deflection of a simply supported beam subjected to a uniformly distributed load (w) over the span is

40 / 50

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

41 / 50

41. The maximum bending moment caused by a moving load on a fixed-end beam occurs

42 / 50

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

43 / 50

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

44 / 50

44. If α is the coefficient of linear expansion, T is the rise in temperature, then thermal stress is given by

45 / 50

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

46 / 50

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

47 / 50

47. Bending moment diagram of simply supported beam with a point load at the centre of the span is

48 / 50

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

49 / 50

49. The maximum bending moment caused by a moment M applied at a distance 'a' from one end on a simply supported beam is.... (where L=span, a>L/2)

50 / 50

50. The moment of inertia of a triangular section b x h about the c-g is

Please provide accurate information so we can send your Achievement Certificate by mail.

Your score is

Share your achievement!

LinkedIn Facebook
0%

Please provide your feedback.

Thank you for your valuable feedback.

Subscribe
Notify of
guest
0 Comments
Scroll to Top