Strength Of Materials Miscellaneous


Strength Of Materials Miscellaneous

Strength Of Materials

  1. A concentrated load P acts on a simply supported beam of span L at a distance L/3 from the left support. The bending moment at the point of application of the load is given by









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    RA + RB =P

    RA =
    2P
    3

    RB =
    P
    3

    BMx = RA x– P (x–L/3)
    BMx=L/3 = RA
    L
    - P
    L
    +
    L
    = RA
    L
    3333

    BM =
    2PL
    9

    Correct Option: D


    RA + RB =P

    RA =
    2P
    3

    RB =
    P
    3

    BMx = RA x– P (x–L/3)
    BMx=L/3 = RA
    L
    - P
    L
    +
    L
    = RA
    L
    3333

    BM =
    2PL
    9


  1. For a simply supported beam on two end supports, the bending moment is maximum









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    Bending moment is maximum where shear force is zero.

    Correct Option: C

    Bending moment is maximum where shear force is zero.



  1. The State of stress at a point, for a body in place stress, is shown in the figure below. If the minimum principal stress is 10 kPa, then the normal stress σs (in kPa) is









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    σx = 100 kPa, τxy = 50 kPa
    Minimum principal stress

    By squaring

    2500 +
    σy2
    - 50σy + 2500 = 1600 +
    σy2
    + 40σy
    44

    ∴ 90 σy = 3400
    σy = 37.78 MPa

    Correct Option: C

    σx = 100 kPa, τxy = 50 kPa
    Minimum principal stress

    By squaring

    2500 +
    σy2
    - 50σy + 2500 = 1600 +
    σy2
    + 40σy
    44

    ∴ 90 σy = 3400
    σy = 37.78 MPa


  1. The state of stress at a point is σx = σy = σz = τxz = τzx = τyx = τzy= 0 and τxy = τyx = 50 MPa. The maximum normal stress (in MPa) at that point is ______.









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    The state of stress is pure shear
    ∴ σ1 = –σ2 = τ = 50 MPa.
    σmax = 50 MPa

    Correct Option: A

    The state of stress is pure shear
    ∴ σ1 = –σ2 = τ = 50 MPa.
    σmax = 50 MPa



  1. The state of stress at a point on an element is shown in figure (a). The same state of stress is shown in another coordinate system in figure (b).

    The components (τxx, τyy, τxy,) are given by









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    σθ =
    σx + σy
    +
    σx - σy
    cos2θ + τxysine2θ
    22

    Here θ = - 45
    σθ = Txy
    σx = p
    σy = - p
    σθ =Txy =
    P + P
    +
    P - P
    cos90° = 0
    22

    When θ = + 45
    σθ =
    P - P
    +
    P + P
    cos90°
    22

    When θ = 45° Tθ = Txy
    Tθ =
    σx - σy
    sin2θ - Txy cos2θ
    2

    Tθ = Txy =
    P + P
    sin90° = P
    2

    ∴ Txx, Tyy, Txy = 0, 0, p

    Correct Option: B


    σθ =
    σx + σy
    +
    σx - σy
    cos2θ + τxysine2θ
    22

    Here θ = - 45
    σθ = Txy
    σx = p
    σy = - p
    σθ =Txy =
    P + P
    +
    P - P
    cos90° = 0
    22

    When θ = + 45
    σθ =
    P - P
    +
    P + P
    cos90°
    22

    When θ = 45° Tθ = Txy
    Tθ =
    σx - σy
    sin2θ - Txy cos2θ
    2

    Tθ = Txy =
    P + P
    sin90° = P
    2

    ∴ Txx, Tyy, Txy = 0, 0, p