Strength Of Materials Miscellaneous


Strength Of Materials Miscellaneous

Strength Of Materials

  1. The three-dimensional state of stress at a point is given by

    The shear stress on the x-face in y-direction at the same point is then equal to









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    Correct Option: C


  1. A large uniform plate containing a rivet hole is subjected to uniform uniaxial tension of 95 MPa. The maximum stress in the plate is











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    σ =
    P
    A

    P = σ A = 95 × 106 × 10 × 10–2 t
    σ =
    P
    =
    95 × 106 × 10 × 10–2 t
    = 190 MPa
    A(10 × 10-2 - 5 × 10–2)t

    Correct Option: B


    σ =
    P
    A

    P = σ A = 95 × 106 × 10 × 10–2 t
    σ =
    P
    =
    95 × 106 × 10 × 10–2 t
    = 190 MPa
    A(10 × 10-2 - 5 × 10–2)t



  1. At a point in a stressed body the state of stress on two planes 45° apart is as shown below. Determine the two principal stresses in MPa.










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    σx = 8 MPa
    τxy = 3MPa
    σn = 2 MPa
    θ = 45°

    σn =
    σx + σy
    +
    σx - σy
    cos2θ - τxysin2θ
    22

    2 =
    8 + σy
    +
    8 - σy
    (0) - 3sin(90)
    22

    ( σy = 2 MPa )
    σ1 , 2 =
    σx + σy
    + √
    σx - σy
    ² + τ²xy
    g2

    =
    8 + 2
    ± √
    8 - 2
    ² + 32
    22

    = 5 ± 4.242
    σ1 / 2 = 9.242, 0.758 MPa

    Correct Option: D


    σx = 8 MPa
    τxy = 3MPa
    σn = 2 MPa
    θ = 45°

    σn =
    σx + σy
    +
    σx - σy
    cos2θ - τxysin2θ
    22

    2 =
    8 + σy
    +
    8 - σy
    (0) - 3sin(90)
    22

    ( σy = 2 MPa )
    σ1 , 2 =
    σx + σy
    + √
    σx - σy
    ² + τ²xy
    g2

    =
    8 + 2
    ± √
    8 - 2
    ² + 32
    22

    = 5 ± 4.242
    σ1 / 2 = 9.242, 0.758 MPa


  1. A thin cylinder of 100 mm internal diameter and 5 mm thickness is subjected to an internal pressure of 10 MPa and a torque of 2000 Nm. Calculate the magnitudes of the principal stresses.











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    di = o.1 m, do = di + 2t
    t = 0.005 m, do = 0.11 m
    T = 2000 Nm
    P = 10 MPa

    σc =
    pdi
    =
    10 × 106 × 0.1
    = 50 MPa
    4t4 × 0.005

    σc =
    pdi
    =
    10 × 106 × 0.1
    = 100 MPa
    2t2 × 0.005

    T
    =
    τ
    Jr

    τ =
    Tr
    J


    = 200 ×
    0.11
    2
    π
    (0.114 - 0.14)
    32

    σ1 , 2 =
    σx + σy
    ± √
    σx - σy
    ² + τ²xy
    22

    =
    50 + 100
    ± √
    50 - 100
    ² + 24.142
    22

    = 75 ± 34.75
    = 109.75 & 40.25 MPa

    Correct Option: A

    di = o.1 m, do = di + 2t
    t = 0.005 m, do = 0.11 m
    T = 2000 Nm
    P = 10 MPa

    σc =
    pdi
    =
    10 × 106 × 0.1
    = 50 MPa
    4t4 × 0.005

    σc =
    pdi
    =
    10 × 106 × 0.1
    = 100 MPa
    2t2 × 0.005

    T
    =
    τ
    Jr

    τ =
    Tr
    J


    = 200 ×
    0.11
    2
    π
    (0.114 - 0.14)
    32

    σ1 , 2 =
    σx + σy
    ± √
    σx - σy
    ² + τ²xy
    22

    =
    50 + 100
    ± √
    50 - 100
    ² + 24.142
    22

    = 75 ± 34.75
    = 109.75 & 40.25 MPa



  1. A circular rod of diameter d and length 3d is subjected to a compressive force F acting at the top point as shown below. Calculate the stress at the bottom most support point A










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    Stress due to Axial force

    σa =
    F
    =
    F
    =
    4F
    (compressive)
    A(π / 4)d2πd2

    Stress due to bending:
    σb =
    My
    =
    Fd
    ×
    d
    =
    16F
    (tensile)
    22
    I
    π
    d4πd2
    64

    Combined stress:
    σr = σa + σb
    σr =
    -4F
    +
    16F
    =
    12F
    πd2πd2πd2

    σr =
    12F
    πd2

    Correct Option: A


    Stress due to Axial force

    σa =
    F
    =
    F
    =
    4F
    (compressive)
    A(π / 4)d2πd2

    Stress due to bending:
    σb =
    My
    =
    Fd
    ×
    d
    =
    16F
    (tensile)
    22
    I
    π
    d4πd2
    64

    Combined stress:
    σr = σa + σb
    σr =
    -4F
    +
    16F
    =
    12F
    πd2πd2πd2

    σr =
    12F
    πd2