Strength Of Materials Miscellaneous


Strength Of Materials Miscellaneous

Strength Of Materials

  1. In a simply-supported beam loaded as shown below, the maximum bending moment in Nm is










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    Taking moment about A,
    100 × .5 + 10 = RB
    RB = 60 N
    ∴ RA = 100 – 60 = 40N

    Correct Option: B


    Taking moment about A,
    100 × .5 + 10 = RB
    RB = 60 N
    ∴ RA = 100 – 60 = 40N


  1. A free bar of length/ is uniformly heated from 0°C to a temperature t°C, α is the coefficient of linear expansion and E the modulus of elasticity. The stress in the bar is









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    For thermal stress to be developed there must be constraint in the system to oppose. So strain develops but there is no thermal stress.

    Correct Option: C

    For thermal stress to be developed there must be constraint in the system to oppose. So strain develops but there is no thermal stress.



  1. Determine the temperature rise necessary to induce buckling in a 1 m long circular rod of diameter 40 mm shown in the figure below. Assume the rod to be pinned at its ends and the coefficient of thermal expansion as 20 × 10–6/°C. Assume uniform heating of the bar.









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    Let Bucking load be P
    δl = αΔTL

    ∴ ΔT =
    δl
    - (i)
    αL

    We know:
    δl =
    PL
    ⇒ =
    AEδl
    - (ii)
    AEL

    Pcolumn =
    π²EI
    - (iii)[Both ends hinged]

    Compare equation (ii) + (iii)
    AE
    δl
    =
    π²EI
    L

    Sl =
    π²l
    - (iv)
    LA

    Putting the value of equation (iv) in equation (i)
    ΔT =
    π²I
    1
    =
    π²I
    LAαLL²Aα

    ΔT =  π² ×
    π
    × (0.040)4
    64
    1³ ×
    π
    × (0.040)² × (20 × 10-6)
    4

    ΔT = 49.35°C

    Correct Option: A


    Let Bucking load be P
    δl = αΔTL

    ∴ ΔT =
    δl
    - (i)
    αL

    We know:
    δl =
    PL
    ⇒ =
    AEδl
    - (ii)
    AEL

    Pcolumn =
    π²EI
    - (iii)[Both ends hinged]

    Compare equation (ii) + (iii)
    AE
    δl
    =
    π²EI
    L

    Sl =
    π²l
    - (iv)
    LA

    Putting the value of equation (iv) in equation (i)
    ΔT =
    π²I
    1
    =
    π²I
    LAαLL²Aα

    ΔT =  π² ×
    π
    × (0.040)4
    64
    1³ ×
    π
    × (0.040)² × (20 × 10-6)
    4

    ΔT = 49.35°C


  1. A frame of two arms of equal length L is shown in the adjacent figure. The flexural rigidity of each arm of the frame is El. The vertical deflection at the point of application of load P is









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    EI
    d2y
    = - Mx
    dx2

    or Mx = – P (L–x)
    ∴ EI
    d2y
    = P (L–x)
    dx2

    Integrating two times and
    puting x = L, we get
    y =
    PL3
    3EI

    U =
    P2L3
    +
    P2L3
    =
    4P2L3
    2EI6EI6EI

    1
    × P × deflection =
    4P2L3
    26EI

    or Deflection =
    4P2L3
    6EI

    Correct Option: D

    EI
    d2y
    = - Mx
    dx2

    or Mx = – P (L–x)
    ∴ EI
    d2y
    = P (L–x)
    dx2

    Integrating two times and
    puting x = L, we get
    y =
    PL3
    3EI

    U =
    P2L3
    +
    P2L3
    =
    4P2L3
    2EI6EI6EI

    1
    × P × deflection =
    4P2L3
    26EI

    or Deflection =
    4P2L3
    6EI



  1. Two identical cantilever beams are supported as shown, with their free ends in contact through a rigid roller. After the load P is applied, the free ends will have









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    As it is rigid roller deflection must be same because after deflection they also will be in contact but slope unequal.

    Correct Option: A

    As it is rigid roller deflection must be same because after deflection they also will be in contact but slope unequal.