Mechanical and structural analysis miscellaneous


Mechanical and structural analysis miscellaneous

Mechanics and Structural Analysis

  1. A uniform beam weighing 1800 N is supported at E and F by cable ABCD. Determine the tension (in N) in segment AB of this cable (correct to 1-decimal place). Assume the cables ABCD, BE and CF to be weightless.









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    Taking Moment about A.

    T3 =
    1800 × 1.25
    = 1125 N
    2

    T4 =
    1800 × 0.75
    = 675 N
    2

    We get, VB × 4.5 = (1125 × 1.5 + 675 × 3.5)
    ⇒ VB = 900 kN ...(i)
    ⇒ VA = (1125 + 675 – 900) = 900 kN
    M1, beam = (VA × 1.5) = 900 × 1.5 = 1350 Nm
    M2, beam = (VA × 3.5 – 1125 × 2)
    = (900 × 3.5 – 2250) = 900 Nm
    Taking bending moment about point (i) [as we know that bending moment at every point in the cable is zero]
    ⇒ Hy1 = M1, beam = 1350 ...(ii)
    Taking bending moment about point (ii)
    ⇒ Hy2 = 900
    ⇒ H =
    900
    = 900 N
    1

    ⇒ 900 y1 = 1350
    ∴ y1 =
    1350
    = 1.5 m ....(iii)
    900

    ∴ θ1 = tan-1
    y1
    = tan-1
    1.5
    = 45
    1.51.5

    θ2 = tan-1
    y1 - y2
    = tan-1
    1.5 - 1
    = 14.03
    22

    From Lamis Theorem
    T1
    =
    1125
    sin(90 + θ2)sin{[180 - (θ1 + θ2)]}

    ⇒ T1 =
    1125sin(90 + 14.03)
    = 1272.91
    sin[180 - (45 + 14.03)]

    Correct Option: C


    Taking Moment about A.

    T3 =
    1800 × 1.25
    = 1125 N
    2

    T4 =
    1800 × 0.75
    = 675 N
    2

    We get, VB × 4.5 = (1125 × 1.5 + 675 × 3.5)
    ⇒ VB = 900 kN ...(i)
    ⇒ VA = (1125 + 675 – 900) = 900 kN
    M1, beam = (VA × 1.5) = 900 × 1.5 = 1350 Nm
    M2, beam = (VA × 3.5 – 1125 × 2)
    = (900 × 3.5 – 2250) = 900 Nm
    Taking bending moment about point (i) [as we know that bending moment at every point in the cable is zero]
    ⇒ Hy1 = M1, beam = 1350 ...(ii)
    Taking bending moment about point (ii)
    ⇒ Hy2 = 900
    ⇒ H =
    900
    = 900 N
    1

    ⇒ 900 y1 = 1350
    ∴ y1 =
    1350
    = 1.5 m ....(iii)
    900

    ∴ θ1 = tan-1
    y1
    = tan-1
    1.5
    = 45
    1.51.5

    θ2 = tan-1
    y1 - y2
    = tan-1
    1.5 - 1
    = 14.03
    22

    From Lamis Theorem
    T1
    =
    1125
    sin(90 + θ2)sin{[180 - (θ1 + θ2)]}

    ⇒ T1 =
    1125sin(90 + 14.03)
    = 1272.91
    sin[180 - (45 + 14.03)]


  1. A uniform beam (EI = constant) PQ in the form of a quartercircle of radius R is fixed at end P and free at the end Q, where a load W is applied as shown. The vertical downward displacement, δq, at the loaded point Q is given by: δq =
    β
    WR3
    EI

    Find the value of b(correct to 4-decimal places).









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    Correct Option: A



  1. All members in the rigid-jointed frame shown are prismatic and have the same flexural stiffness EI. Find the magnitude of the bending moment at Q (in kNm) due to the given loading.









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    Correct Option: D



  1. The pin-jointed 2-D truss is loaded with a horizontal force of 15 kN at joint S and another 15kN vertical force at joint U, as shown. Find the force in member RS (in kN) and report your answer taking tension as positive and compression as negative.









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    ∑ MT = 0
    ⇒ Rv × 8 – 15 × 4 + 15 × 4 = 0
    ∴ Rv = 0
    Take moment about V, MV = 0
    ⇒ RH × 4 = 0
    ∴ RH = 0
    We know that if two members meet at a joint which are not col-linear and also there is no external forces acting on that joint then both members will carry zero forces.
    ∴ FQV = FQR = 0
    Now, consider joint R
    ∑ Fy = 0

    ⇒ FRU sin 45º = 0
    ⇒ FRU = 0
    Now, 0 ∑ Fx = ⇒ FRS + FRU cos 45º = 0
    ⇒ FRS + FRU cos 45º = 0
    ∴ FRS = 0
    So, force is member is “RS” will be zero.

    Correct Option: A


    ∑ MT = 0
    ⇒ Rv × 8 – 15 × 4 + 15 × 4 = 0
    ∴ Rv = 0
    Take moment about V, MV = 0
    ⇒ RH × 4 = 0
    ∴ RH = 0
    We know that if two members meet at a joint which are not col-linear and also there is no external forces acting on that joint then both members will carry zero forces.
    ∴ FQV = FQR = 0
    Now, consider joint R
    ∑ Fy = 0

    ⇒ FRU sin 45º = 0
    ⇒ FRU = 0
    Now, 0 ∑ Fx = ⇒ FRS + FRU cos 45º = 0
    ⇒ FRS + FRU cos 45º = 0
    ∴ FRS = 0
    So, force is member is “RS” will be zero.



Direction: A rigid beam is hinged at one end and supported on linear elastic springs (both having a stiffness of ‘k’) at points ‘1’ and ‘2’ and an inclined load acts at ‘2’, as shown.

  1. If the load P equals 100 kN, which of the following options represents forces R1 and R2 in the springs at points ‘1’ and ‘2’?









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    At 1,

    R1 = kδ1 =
    2p
    =
    2 × 100
    = 40 kN
    55

    At 2,
    R2 = kδ2 =
    4p
    = 80 kN
    5

    Correct Option: D

    At 1,

    R1 = kδ1 =
    2p
    =
    2 × 100
    = 40 kN
    55

    At 2,
    R2 = kδ2 =
    4p
    = 80 kN
    5