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RCC Design Test 2
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RCC Design Test 2
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  • Question 1/10
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    A two way RC slab is provided with steel of total area 1500 mm2 in the shorter direction. If the slab corners with both the edges discontinuous are restrained, the torsional reinforcement required at the corner in each layer is (in mm2 up to 2 decimal places) ______
    Solutions

    Concept:

    Torsional Reinforcement detailing in Slab:-

    Torsional reinforcement is provided in the form of a grid or mesh both at the top and bottom of the slab. IS 456: 2000 recommends that the torsional reinforcement grid should extend beyond the edge for a distance not less than 20% of shorter span. The total area of torsional steel provided in each of the four layers should not be less than:-

    1. \(0.75\;{A_{stx}}\;\)if both the meeting edges are discontinuous.

    2. \(0.375\;{A_{stx}}\) if one of the two meeting edges, one in continuous and other discontinuous

    Here, \({A_{stx}}\) denotes are of flexural steel required for maximum mid span moment in the short direction.

    No torsional reinforcement is required if both the meeting edges are continuous.

    Calculation:

    Ast-x = 1500 mm2

    ∴ Torsional R/F in each layer = 0.75 × 1500 = 1125 mm2
  • Question 2/10
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    The minimum lap length required for reinforcing bars in flexural  tension is α times the bar diameter. The value of α is
    Solutions

    Concept:

    Lap splicing is done by overlapping the bars over a certain length that makes the transfer of force from terminating bar to the connecting bar.

    The straight length of the lap should not be less than 15 times the bar diameter or 200 mm whichever is more. The lap length must at least be equal to development length.

    In flexural and direct tension, minimum lap length should be 30 times the bar diameter. In compression minimum lap length should be twenty four times the bar diameter.

  • Question 3/10
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    As per IS 456 : 2000, Which of the following type of torsion is considered in design?
    Solutions

    Concept:

    Torsional moment exist along with bending moment as well as shear force, axial force and generally shear stresses are induced in the beam due to torsion.

    Equilibrium torsion:- The torsion induced in an RCC member due to eccentric loading with respect to the center is called equilibrium torsion.

    Equilibrium Torsion in beam 2 due to load P shown above.

    Compatibility Torsion: This type of torsion is induced due to the need of the member to undergo a certain angle of  twist to maintain the compatibility conditions. The twisting moment developed is statically indeterminate.

     

    Compatibility Torsion/ Secondary Torsion/ Statically Indeterminate Torsion in 2 and 3 due to load P shown above.

    Explanation:

    If torsional stiffness of member is neglected the member is designed for bending moment only and shear force is assumed to cater for compatibility torsion.

    Thus the design is done only for equilibrium torsion.

  • Question 4/10
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    A beam is subjected to factored shear force of 50 kN, Factored Bending Moment of 100 kN-m and Factored Torsional Moment of 150 KN-m. Find the equivalent factored shear force (KN) developed for this beam as per as IS 456 : 2000 Take width of the Beam as 300 mm.
    Solutions

    Equivalent shear force (Vue) is given by

    \(\begin{array}{l}{V_{ue}} = {V_u} + \frac{{1.6{T_u}}}{B}\\{V_{ue}} = 50 + \frac{{1.6 \times 150}}{{0.300}}\end{array}\)

    Vue = 850 kN
  • Question 5/10
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    A RCC member of total width 250 mm and effective depth 450 mm is reinforced with Fe 415 bars. If there is a factored shear force of 200 kN and bending moment of 50 kN-m and there is compression confinement the maximum diameter of bars required considering anchorage as 400 mm is

    Consider M20, τbd = 1.2 MPa (for Fe 415 bar)

    Solutions

    Concept:

    Development Length \(\left( {{\ell _d}} \right) = \frac{{0.87\;{f_y}}}{{4\;{\tau _{bd}}}}\)

    Also,

    \({\ell _d} \le 1.3\frac{{{M_u}}}{{{V_u}}} + {\ell _0}\)             (When there is compression confinement)

    Where,

    Mu = Ultimate MOR at a section considering stress in all bars as 0.87 fy

    Vu = Factored shear force at the point of zero moment.

    0 = Anchorage length

    Calculation:

    Mu = 50 kN – m, Vu = 200 kN, ℓ0 = 400 mm

    \(\therefore {\ell _d} \le 1.3 \times \frac{{50}}{{200}} + \frac{{400}}{{1000}} = 0.725\;m\)

    d ≤ 725 mm

    At limiting condition,

    d = 725 mm

    Also,

    \({\ell _d} \ge \frac{{0.87\;{f_y}\;\phi }}{{4\;{\tau _{bd}}}} \Rightarrow 725 \ge \frac{{0.87 \times 415 \times \phi }}{{4 \times 1.2}}\)

    ϕ 9.638 mm  

    Thus the maximum bar dia that can be provided is 9 mm.

    Mistake Point:

    The value of bond stress is given for Fe 415 bar and we need not add 60 % in the given value.

    Important Point:

    In case of simple support or the places where there is no compression confinement, tension R/F should be limited to a diameter, such that

    \({\ell _d} \le \frac{{{M_u}}}{{{V_u}}} + {\ell _0}\)

  • Question 6/10
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    A simply supported one-way slab of effective depth 400 mm is required to resist the ultimate moment of 37 kN-m/m, if 10 mm diameter main bar is used in the slab, the spacing of the main bar required will be?

    (Assume Grade of concrete and steel to be M-25 and Fe-500 respectively)
    Solutions

    Concept:

    Area of steel required will be:

    \({A_{st\left( {req} \right)}} = \frac{{0.5{f_{ck}}}}{{{f_y}}}\left( {1 - \sqrt {1 - \frac{{4.6{M_u}}}{{{f_{ck}}b{d^2}}}} } \right) \times bd\)

    Where,

    Mu = ultimate moment of the slab, b = width of the slab, and d = effective depth of the slab,

    fck and fy have usual meanings

    Spacing of the bar = \(\frac{{1000}}{{{{\rm{A}}_{{\rm{st}}}}}} \times {{\rm{A}}_\phi }\)

    Minimum Area of steel in slab = 0.12% of cross-sectional area of slab = 0.0012bd

    Maximum spacing of main bar in slab = 3d or 300 mm whichever is lesser.

    Calculation:

    Mu = 37 kN-m, b = 1000 mm, and d = 400 mm

    \({{\rm{A}}_{{\rm{st}}\left( {{\rm{req}}} \right)}} = \frac{{0.5 \times 25}}{{500}}\left( {1 - \sqrt {1 - \frac{{4.6 \times 37 \times {{10}^6}}}{{25 \times 1000 \times {{400}^2}}}} } \right)1000 \times 400 = 215{\rm{\;m}}{{\rm{m}}^2}/{\rm{m}}\)

    But minimum Area of steel should be,

    \({\rm{As}}{{\rm{t}}_{{\rm{min}}}} = \frac{{0.12}}{{100}} \times 1000 \times 400 = 480{\rm{m}}{{\rm{m}}^2}/{\rm{m}}\)

    Hence the spacing of the bar should be,

    \({{\rm{A}}_\phi } = \frac{{\rm{\pi }}}{4} \times 10 \times 10 = 78.54{\rm{\;m}}{{\rm{m}}^2}\)

    \({\rm{Spacing}} = \frac{{1000}}{{480}} \times 78.54 = 163.62{\rm{\;mm}}\)

    Check for spacing:

    Maximum spacing should be lesser of 3d or 300 mm whichever is lesser.

    ∴ Spacing = 3 x 400 = 1200 mm or 300 mm whichever is lesser.

    Hence provide 8ϕ -160 mm c/c main bar in the slab.

  • Question 7/10
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    An RC beam is subjected to a factored bending moment of 200 kN-m and a factored torque of 150 kN m. The size of the beam is 250 mm wide with an overall depth of 500 mm and an effective cover of 25 mm. The area of Fe 415 reinforcement provided on the flexural compression side is
    Solutions

    Concept:

    Equivalent Bending Moment:

    Me1 = Mu + Mt

    \({M_t} = \frac{{{T_u}}}{{1.7}}\left( {1 + \frac{D}{b}} \right)\)

    Where, Me1 = equivalent factored B.M, Tu = Factored Torsional Moment, D = Overall Depth of section, b = Width of the section

    Design for Bending:

    • Longitudinal Reinforcement shall be designed to resist equivalent B.M  Me1.
    • Design the cross-section either as singly reinforced or doubly reinforced depending on the value of Me1 & cross-section size. For singly reinforced section,
      \({M_{e1}} = 0.87\;{f_y}\;Ast\;\left( {d - \frac{{{f_y}\;{A_{st}}}}{{{f_{ck}}\;b}}} \right)\)
    • If |Mt| > |Mu|, i.e. the numerical value of Mt exceeds the numerical value of moment Mu, then longitudinal reinforcement shall be provided on the flexural compression side for moment Me2.
      Me2 = |Mt| - |Mu|
      Also, Me2 = 0.87 fy Ast (d – d’)
      Ast = Tensile reinforcement on the flexural compression side
    • If |Mt| < |Mu|, then no need to provide extra reinforcement on the flexural compression side.


    Calculation:

    Mu = 200 kN-m, Tu = 150 kN-m

    \(\therefore {M_t} = \frac{{{T_u}}}{{1.7}}\left( {1 + \frac{D}{b}} \right) = \frac{{150}}{{1.7}}\left( {1 + \frac{{500}}{{250}}} \right) = 264.71\;kN - m\)

    Here, Mt > Mu

    Compression R/F is provided on the flexural compression side for moment Me2.

    Me2 = Mt - Mu = 264.71 – 200 = 64.71 kN-m

    Also, d’ = d = 25 mm.

    Me2 = 0.87 fy Ast (d – d’)

    64.71 × 106 = 0.87 × 415 × Ast (475 - 25)

    ⇒ Ast = 398.28 mm2 ≈ 400 mm2

  • Question 8/10
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    Consider a cantilever beam subjected to gravity load as shown in the figure below.

    It is required to provide development length to both the bars A and B (same diameter). Which of the following statement is/are correct? (Take M 25 and Fe 500)

    Use limit state method and assume permissible bond stress to be 1.4 MPa.

    Solutions

    Concept:

    Development length required by limit state method is:

    \({{\rm{L}}_{\rm{d}}} = \frac{{\phi \times 0.87 \times {{\rm{f}}_{\rm{y}}}}}{{4 \times {{\rm{\tau }}_{{\rm{b}}{{\rm{d}}_{{\rm{perm}}}}}}}}\)

    Where

    ϕ = Bar diameter, fy = Grade of steel, and \({{\rm{\tau }}_{{\rm{b}}{{\rm{d}}_{{\rm{perm}}}}}} = {\rm{Permissible\;bond\;stress}}\) 

    For bars in compression, the permissible bond stress is increased by 25% and for HYSD, CTD, TMT bars, the bond stress is additionally increased by 60%.

    Calculation:

    For bar A:

    \({\left( {{{\rm{L}}_{\rm{d}}}} \right)_{\rm{A}}} = \frac{{{\phi _{\rm{A}}} \times 0.87 \times {{\rm{f}}_{\rm{y}}}}}{{4 \times {{\rm{\tau }}_{{\rm{b}}{{\rm{d}}_{\rm{A}}}}}}}\)

    As bar A is in tension but it should be increased by 60% as the bar used is HYSD bar.

    \({{\rm{\tau }}_{{\rm{b}}{{\rm{d}}_{\rm{A}}}}} = 1.4 \times 1.60 = 2.24{\rm{\;N}}/{\rm{m}}{{\rm{m}}^2}\)

    Development length for bar A is given by:

    \({\left( {{{\rm{L}}_{\rm{d}}}} \right)_{\rm{A}}} = \frac{{{\phi _{\rm{A}}} \times 0.87 \times 500}}{{4 \times 1.4 \times 1.60}} = 48.55 \times {\phi _{\rm{A}}} = 48.55{\rm{\;}}\phi \)

    For bar B:

    \({\left( {{L_d}} \right)_B} = \frac{{{\phi _B} \times 0.87 \times {f_y}}}{{4{\tau _{b{d_B}}}}}\)

    As bar B is in compression therefore it should be increased by 25% apart from increased by 60% due to bar of type HYSD.

    \({{\rm{\tau }}_{{\rm{b}}{{\rm{d}}_{\rm{B}}}}} = 1.4 \times 1.6 \times 1.25 = 2.8{\rm{\;N}}/{\rm{m}}{{\rm{m}}^2}\)

    \({\left( {{{\rm{L}}_{\rm{d}}}} \right)_{\rm{B}}} = \frac{{\phi \times 0.87 \times 500}}{{4 \times 1.4 \times 1.6 \times 1.25}} = 38.84\;\phi \)

     (Ld)A > (Ld)B

    Hence more length of reinforcement is required for reinforcement marked A as compared to reinforcement marked B.
  • Question 9/10
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    The total width of a one-way slab made of RC is 2000 mm and the thickness is 200 mm with an effective cover of 20 mm. It is reinforced with mild steel. The maximum dia of the reinforcing bars and the minimum steel requirement in either direction of the slab is
    Solutions

    Concept:

    Reinforcement Requirements in One Way Slab:-

    Mild steel requirement in either direction of the slab shall not be less than 0.15% of the total cross-sectional area (bD). However for HYSD bars in either direction, the reinforcement shall not be less than 0.12% of the gross cross-sectional area.

    Maximum dia of reinforcing bars shall not exceed \(\frac{1}{8}\)of the total thickness of slab. { e.g. t = 80 mm ϕ = 10 mm}

    Calculation:-

    b = 2000 mm, D = 200 mm

    Minimum percentage of mild steel = 0.15% of total cross-sectional area

    \( = \frac{{0.15}}{{100}} \times 2000 \times 200 = 600\;m{m^2}\)

    Also, Maximum thickness of reinforcing bars = \(\frac{1}{8} \times \) total thickness \( = \frac{1}{8} \times 200 = 25\;mm\)
  • Question 10/10
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    The following assumptions are made considering the analysis of a two-way slab using the yield line method:

    P) The reinforcement steel undergoes plastic deformation at failure along the yield line.

    Q) The slab separates into segments and each segment behaves plastically.

    R) The bending and twisting moment are uniformly distributed along a yield line.

    Choose the correct code:
    Solutions

    Concept:

    The attainment of the ultimate flexural strain at one cross-section doesn’t lead to the collapse of the slab. The yield line analysis is carried out to economize the structure. It is based on the upper bound theory. Assumptions of yield line analysis are:-

    (i) The reinforcing steel is fully yielded along the yield line at failure and undergoes plastic deformation.

    (ii) The slab separates into segments by the yield lines. The individual segments behave elastically.

    (iii) Elastic deformations are negligible compared to plastic deformations.

    (iv) The Bending & Twisting moment are uniformly distributed along the yield line and have the maximum value provided by the ultimate moment capacity.

    Explanation:

    P is true because we have plastic deformation along yield line.

    Q is false as each segment behaves elastically.

    R is true and it follows from the assumption iv listed above.

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