RCDC L shape column design as per IS:456

One of our would-be client wants to get a L shape RCC column design computation done in RCDC as per IS:456 for checking purpose.

If some readyment compuation for any size L shape column is availablepl share it.

  • Hi,

    I just quickly created a file with very basic details and load case with a L shape column. Please see if this helps. I believe you will be able to extract drawings and reports from the attached RCDC file. please let us know if you need any more info.

    https://communities.bentley.com/cfs-file/__key/communityserver-discussions-components-files/5932/Structure1_2D00_Column_2D00_1.rcdx3276.Structure1.STD

    Thanks & Regards,
    Abhisek Mandal
    Global Technical Support

  • Dear Sir
    Thanks for prompt reply.
    However since we do not have RCDC installed in our computer we will not be able to run.
    We therefore request you to kindly run and there after send some text/xls file so that our client go through that to get themselves satisfied.

    Thanks & best regards

    K Roy Chowdhury
    Technology Development Centre
    A-73, New Raipur,
    Kolkata - 700 084, India.
    Mobile : 98302 77706
    Office :990 334 7770
    www.tdcindia.com

    Disclaimer: The information contained in this communication is intended
    solely for the individual or entity to which it is addressed. It may contain confidential and/or legally privileged information. Any review,
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    On Wednesday, 14 July, 2021, 03:59:17 pm IST, Abhisek M <bounce-acf23087-849f-4d60-bda1-baad225ed835@communities.bentley.com> wrote:


    Update from Bentley Communities

    [AUTOMATED MESSAGE; if there is a link below, please follow that if you wish to respond to this Communities message.]


    RE: RCDC L shape column design as per IS:456

    Abhisek M

    Hi,

    I just quickly created a file with very basic details and load case with a L shape column. Please see if this helps. I believe you will be able to extract drawings and reports from the attached RCDC file. please let us know if you need any more info.

    communities.bentley.com/.../Structure1_2D00_Column_2D00_1.rcdxcommunities.bentley.com/.../3276.Structure1.STD


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  • Dear Sir
    Thanks for prompt reply.
    However since we do not have RCDC installed in our computer we will not be able to run.
    We therefore request you to kindly run and there after send some text/xls file so that our client go through that to get themselves satisfied.

    Thanks & best regards

    K Roy Chowdhury
    Technology Development Centre
    A-73, New Raipur,
    Kolkata - 700 084, India.
    Mobile : 98302 77706
    Office :990 334 7770
    www.tdcindia.com

    Disclaimer: The information contained in this communication is intended
    solely for the individual or entity to which it is addressed. It may contain confidential and/or legally privileged information. Any review,
    retransmission, dissemination or other use of, or taking any action in
    reliance on the contents of this information by persons or entities
    other than the intended recipient is strictly prohibited and may be
    unlawful. If you have received this communication by error, please notify us immediately by responding to this email and then delete it from your system. Technology Development Centre attempts to sweep e-mails and attachments for viruses, it does not guarantee that either are virus free and that we accept no liability for any damage sustained as a result of VIRUSES.


    On Wednesday, 14 July, 2021, 03:59:17 pm IST, Abhisek M <bounce-acf23087-849f-4d60-bda1-baad225ed835@communities.bentley.com> wrote:


    Update from Bentley Communities

    [AUTOMATED MESSAGE; if there is a link below, please follow that if you wish to respond to this Communities message.]


    RE: RCDC L shape column design as per IS:456

    Abhisek M

    Hi,

    I just quickly created a file with very basic details and load case with a L shape column. Please see if this helps. I believe you will be able to extract drawings and reports from the attached RCDC file. please let us know if you need any more info.

    communities.bentley.com/.../Structure1_2D00_Column_2D00_1.rcdxcommunities.bentley.com/.../3276.Structure1.STD


    Did this answer your question?

    Verify it as the answer or Reject it as the answer

    View online

     

    You received this notification because you subscribed to the forum.  To unsubscribe from only this thread, go here.

    Flag this post as spam/abuse.

  • clsRCDCInfo:RestoreProjectSchema - ERROR: 3F000: schema "AN_Frame_Assignments" does not exist

  • General Data
    Column No. : C1
    Level : 0m To 7.5m
    Design Code = IS 456 + IS 13920 - 2016
    Grade Of Concrete = M25 N/sqmm
    Grade Of Steel = Fe415 N/sqmm
    Shape = L-Shape
    DF1 = 750 mm
    BF1 = 250 mm
    DF2 = 750 mm
    BF2 = 250 mm
    Outermost Lx = 750 mm
    Outermost Ly = 750 mm
    Clear Floor Height @ B = 7100 mm
    Clear Floor Height @ D = 7100 mm
    No Of Floors = 1
    No Of Columns In Group = 1
    Column Type : UnBraced
    Minimum eccentricity check : One Axis at a Time
    Code defined D/B ratio : 4
    D/B Ratio : 1 <= 4 Hence, Design as Column



    Load Data
    Analysis Reference No. = 5
    Load Combination = [1] : 1.5 (LOAD 1: LOAD CASE 1) +1.5 (LOAD 2: LOAD CASE 2)
    Critical Location = Top Joint
    Pu = 226.73 kN
    Mux = -18.65 kNm
    Muy = 18.65 kNm
    Vux = 3.36 kN
    Vuy = 3.36 kN




    Minimum Eccentricity Check
    Since Axial Force is compressive, Min. Eccentricity check to be performed
    Most critical case is with Min. Eccentricity check in X-direction
    Minimum Eccentricity Along Lx:
    Minimum Eccentricity = Unsupported Length / 500 + Lx / 30
                    = 39.2 mm
    Minimum Eccentricity > 20 mm
    Mminx = Pu x Minimum Eccentricity
    = 8.89 kNm
    Slenderness Check
    Max Slenderness Ratio(Lx/Ly) = 9.47
    < 60 (Hence Ok)
    Column Is Unbraced Along Lx
    Slenderness Check Along Lx:
                   Effective Length Factor = 1
                   Slenderness Ratio = Effective Length / Lx
    = 9.47, Column not Slender Along Lx
    Column Is Unbraced Along Ly
    Slenderness Check Along Ly:
                   Effective Length Factor = 1
                   Slenderness Ratio = Effective Length / Ly
    = 9.47, Column not Slender Along Ly



    Calculation of Design Moment
    Direction Manalysis Mmin (Abs) Mdesign Mslndx (Abs) Mdesign-final
    A B C E F
    Major Axis - Mux   -18.65 8.89 -18.65 0 -18.65
    Minor Axis - Muy 18.65 --- 18.65 0 18.65

    Where
    A = Moments directly from analysis
    B = Moments due to minimum eccentricity
    C = Maximum of analysis moment and min. eccentricity = Max (A,B)
    E = Moment due to slenderness effect
    F = Final design Moment = Max(C- Top Bottom , D- Top Bottom) + E

     

    Final Critical Design Forces
    Pu = 226.73 kN
    Mux = -18.65 kNm
    Muy = 18.65 kNm

    Resultant Moment (Combined Action)
    Moment Capacity Check
    Pt Calculated = 0.43
    Reinforcement Provided = 12-T12
    Load Angle = Tan-1(Muy/Mux)
    = 225 deg
    MRes = 26.38 kNm
    MCap = 151.35 kNm
    Capacity Ratio = MRes/ MCap
    = 0.17 <= 1
    Design Of Shear
    Design for shear along Lx
    Critical Load Combination = [1] : 1.5 (LOAD 1: LOAD CASE 1) +1.5 (LOAD 2: LOAD CASE 2)
    Design shear force, Vuy = 3.359 kN
    Pu = 226.73
    Deff = 694 mm
    Design shear stress, Tvy = Vuy / (Lyx Deff) N/sqmm
    = 0.0124 N/sqmm
    Pt = 0.217 %
    Design shear strength, Tc = 0.343 N/sqmm
    Shear Strength Enhancement Factor = 1 + 3 x Pu / ( Ag x Fck)
    = 1.0871
    Shear Strength Enhancement Factor (max) = 1.5
    Shear Strength Enhancement Factor = 1.0871
    Enhanced shear strength, Tc-e = 0.3728 N/sqmm
    Design shear check = Tvy < Tc x Enhancement factor
    Link for Shear Design along Lx are not required
     
    Design for shear along Ly
    Critical Load Combination = [1] : 1.5 (LOAD 1: LOAD CASE 1) +1.5 (LOAD 2: LOAD CASE 2)
    Design shear force, Vux = 3.359 kN
    Pu = 226.73
    Beff = 694 mm
    Design shear stress, Tvx = Vux / (Lx x Beff) kN
    = 0.0124 N/sqmm
    Pt = 0.217 %
    Design shear strength, Tc = 0.343 N/sqmm
    Shear Strength Enhancement Factor = 1 + 3 x Pu / (Ly x Lx x Fck)
    = 1.0871
    Shear Strength Enhancement Factor (max) = 1.5
    Shear Strength Enhancement Factor = 1.0871
    Enhanced shear strength, Tc-e = 0.3728 N/sqmm
    Design shear check = Tvx < Tc x Enhancement factor
    Link for Shear Design along Ly are not required



    Design Of Links
    Links in the zone where special confining links are not required
    Normal Links
    Diameter of link = 8 mm
      > Max. longitudinal bar dia / 4
      = 3 mm
    Criterion for spacing of normal links
    Min. Longitudinal Bar dia X 16 = 192 mm
    Min. dimension of column = 750 mm
    Max. 300 mm = 300 mm
     
    Provided spacing = 175 mm
     
     
    Table For Links
    Required Provided
    Normal Design Shear Design Ductile Design Normal Zone Ductile Zone
    Link Dia. 8 --- --- 8 ---
    Spacing 175 --- --- 175 ---


     

    General Data
    Column No. : C1
    Level : 7.5m To 15m
    Design Code = IS 456 + IS 13920 - 2016
    Grade Of Concrete = M25 N/sqmm
    Grade Of Steel = Fe415 N/sqmm
    Shape = L-Shape
    DF1 = 750 mm
    BF1 = 250 mm
    DF2 = 750 mm
    BF2 = 250 mm
    Outermost Lx = 750 mm
    Outermost Ly = 750 mm
    Clear Floor Height @ B = 7100 mm
    Clear Floor Height @ D = 7100 mm
    No Of Floors = 1
    No Of Columns In Group = 1
    Column Type : UnBraced
    Minimum eccentricity check : One Axis at a Time
    Code defined D/B ratio : 4
    D/B Ratio : 1 <= 4 Hence, Design as Column



    Load Data
    Analysis Reference No. = 8
    Load Combination = [1] : 1.5 (LOAD 1: LOAD CASE 1) +1.5 (LOAD 2: LOAD CASE 2)
    Critical Location = Top Joint
    Pu = 70.72 kN
    Mux = -39.32 kNm
    Muy = 39.32 kNm
    Vux = 8.48 kN
    Vuy = 8.48 kN




    Minimum Eccentricity Check
    Since Axial Force is compressive, Min. Eccentricity check to be performed
    Most critical case is with Min. Eccentricity check in X-direction
    Minimum Eccentricity Along Lx:
    Minimum Eccentricity = Unsupported Length / 500 + Lx / 30
                    = 39.2 mm
    Minimum Eccentricity > 20 mm
    Mminx = Pu x Minimum Eccentricity
    = 2.77 kNm
    Slenderness Check
    Max Slenderness Ratio(Lx/Ly) = 9.47
    < 60 (Hence Ok)
    Column Is Unbraced Along Lx
    Slenderness Check Along Lx:
                   Effective Length Factor = 1
                   Slenderness Ratio = Effective Length / Lx
    = 9.47, Column not Slender Along Lx
    Column Is Unbraced Along Ly
    Slenderness Check Along Ly:
                   Effective Length Factor = 1
                   Slenderness Ratio = Effective Length / Ly
    = 9.47, Column not Slender Along Ly



    Calculation of Design Moment
    Direction Manalysis Mmin (Abs) Mdesign Mslndx (Abs) Mdesign-final
    A B C E F
    Major Axis - Mux   -39.32 2.77 -39.32 0 -39.32
    Minor Axis - Muy 39.32 --- 39.32 0 39.32

    Where
    A = Moments directly from analysis
    B = Moments due to minimum eccentricity
    C = Maximum of analysis moment and min. eccentricity = Max (A,B)
    E = Moment due to slenderness effect
    F = Final design Moment = Max(C- Top Bottom , D- Top Bottom) + E

     

    Final Critical Design Forces
    Pu = 70.72 kN
    Mux = -39.32 kNm
    Muy = 39.32 kNm

    Resultant Moment (Combined Action)
    Moment Capacity Check
    Pt Calculated = 0.43
    Reinforcement Provided = 12-T12
    Load Angle = Tan-1(Muy/Mux)
    = 225 deg
    MRes = 55.61 kNm
    MCap = 126.19 kNm
    Capacity Ratio = MRes/ MCap
    = 0.44 <= 1
    Design Of Shear
    Design for shear along Lx
    Critical Load Combination = [1] : 1.5 (LOAD 1: LOAD CASE 1) +1.5 (LOAD 2: LOAD CASE 2)
    Design shear force, Vuy = 8.4809 kN
    Pu = 70.72
    Deff = 694 mm
    Design shear stress, Tvy = Vuy / (Lyx Deff) N/sqmm
    = 0.0314 N/sqmm
    Pt = 0.217 %
    Design shear strength, Tc = 0.343 N/sqmm
    Shear Strength Enhancement Factor = 1 + 3 x Pu / ( Ag x Fck)
    = 1.0272
    Shear Strength Enhancement Factor (max) = 1.5
    Shear Strength Enhancement Factor = 1.0272
    Enhanced shear strength, Tc-e = 0.3523 N/sqmm
    Design shear check = Tvy < Tc x Enhancement factor
    Link for Shear Design along Lx are not required
     
    Design for shear along Ly
    Critical Load Combination = [1] : 1.5 (LOAD 1: LOAD CASE 1) +1.5 (LOAD 2: LOAD CASE 2)
    Design shear force, Vux = 8.4809 kN
    Pu = 70.72
    Beff = 694 mm
    Design shear stress, Tvx = Vux / (Lx x Beff) kN
    = 0.0314 N/sqmm
    Pt = 0.217 %
    Design shear strength, Tc = 0.343 N/sqmm
    Shear Strength Enhancement Factor = 1 + 3 x Pu / (Ly x Lx x Fck)
    = 1.0272
    Shear Strength Enhancement Factor (max) = 1.5
    Shear Strength Enhancement Factor = 1.0272
    Enhanced shear strength, Tc-e = 0.3523 N/sqmm
    Design shear check = Tvx < Tc x Enhancement factor
    Link for Shear Design along Ly are not required



    Design Of Links
    Links in the zone where special confining links are not required
    Normal Links
    Diameter of link = 8 mm
      > Max. longitudinal bar dia / 4
      = 3 mm
    Criterion for spacing of normal links
    Min. Longitudinal Bar dia X 16 = 192 mm
    Min. dimension of column = 750 mm
    Max. 300 mm = 300 mm
     
    Provided spacing = 175 mm
     
     
    Table For Links
    Required Provided
    Normal Design Shear Design Ductile Design Normal Zone Ductile Zone
    Link Dia. 8 --- --- 8 ---
    Spacing 175 --- --- 175 ---