Challenge

Project 1

Beam column element

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CONNECTED USER: Shyam Datta



COLUMN DESIGN CALCULATIONS
Project Name : Unassigned
Client Name : Unassigned
Engineer Name : Unassigned
Analysis File : C:\Users\shyam\OneDrive\Desktop\Shyam\project 1.STD
Analysis Last Modified : 9/12/2022 3:09:34 PM
Definitions Of Terms:
All forces in units kN and m
All reinforcement details like area, spacing are mm
Grade Of steel for 6 mm dia. bars is Fe250. It is irrespective of the grade of steel defined by user in column design.
Neutral axis angle for resultant design moment is with respect to local major axis.
1 β = Stiffness proportion factor at joint ( column stiffness/sum of stiffness of all members connected at joint)
2 Δu = Elastically computed first order lateral deflection.(Relative deflections)
3 ε1 = Strain at level considered, Calculated ignoring the stiffening of the concrete in tension zone
4 εm = Average steel strain at level considered
5 acr = Distance from the point considered to the surface of the nearest longitudinal bar
6 Ag = Gross area of the column cross section
7 Ak = Area of confined concrete core
8 Ash = Area of link cross section
9 b = Effective Width of Column in mm
10 B = Width / Smaller Dimension of Column in mm
11 d = Effective Depth of Column in mm
12 D = Depth / Larger Dimension of Column OR Diameter of Circular Column in mm
13 Dk = Diameter Of core measured to the outside of circular link
14 Ec = Modulus of elasticity of concrete
15 Es = Modulus of elasticity of steel
16 FcPerm = Permissible Stress in Concrete required in N/ (sqmm)
17 Fst = Stress in steel
18 FstPerm = Permissible Stress in Steel required in N/ (sqmm)
19 Fck = Characteristic compressive strength of concrete cube in N/sqmm
20 Fy = Yield Stress Of Steel in N/sqmm
21 h = Longer dimension of rectangular link measured to its outer face
22 Hu = Total lateral force acting within the story(Story shear)
23 Hs = Height of the story (Floor height)
24 k = Reduction factor for slenderness moments
25 Max = Additional moment due to slenderness about major axis (Along D)
26 May = Additional moment due to slenderness about minor axis (Along B)
27 Mminx = Moment due to minimum eccentricity along D
28 Mminy = Moment due to minimum eccentricity along B
29 Muv = Moment capacity of web portion of wall as per clause 9.4.2 and Annes A of IS 13920 - 2016
30 Mux = Factored moment Along D (Momemt About Major Axis)
31 Muy = Factored moment Along B (Momemt About Minor Axis)
32 MCap = Moment capacity of section for NA angle at design Pu
33 MRes = Resultant design moment at angle to local major axis
34 Pb = Axial capacity of column along B as defined in 39.7.1.1
35 Pd = Axial capacity of column along D as defined in 39.7.1.1
36 Pu = Factored axial force
37 Puz = Axial load on column as defined in 39.6
38 Pu_Total = Sum of Axial loads on all column in the story (Gravity Load)
39 Q = Stability Index (factor for checking sway/ non sway condition for a given story)
40 S = Link Spacing
41 Shear Strength Enhancement Factor = Multiplying factor for shear strength of concrete as per 40.2.2
42 Vur = Factored resultant shear force acting on the column
43 Vux = Factored shear force Along B
44 Vuy = Factored shear force Along D
45 Wcr = Surface Crack Width
46 WcrPerm = Permissible Crack Width required in mm
47 β = It is a Neutral Axis angle corresponding to load angle to find out MCap



Code References:
IS 456
ELEMENT CLAUSE / table
1 Max area of reinforcement : 26.5.3.1-a & b
2 Min area of reinforcement : 26.5.3.1-a & b
3 Min number of bars : 26.5.3.1-c
4 Minimum Eccentricity Calc : 25.4 & 39.2
5 Effective Length : 25.2
6 Slenderness Moments : 25.3 & 39.7
7 Design for axial loads : 39.3
8 Design for axial loads And uniaxial bending : 39.5
9 Design for axial loads And Biaxial bending : 39.6
10 Design of horizontal links : 26.5.3.2
11 Design shear strength : 40.2
12 Stiffness Proportion Factor, β : E-1
13 Stability(Index, Q) : E -2
14 Crack width calculation : 3.8
15 Multiplying factor to Beam Stiffness for effective length calculation : SP 24 1983 APPENDIX D
IS 13920 - 2016
ELEMENT CLAUSE / table
1 Spacing of special confining reinforcement : 10.4 and 7.6
2 C/s area of special confining reinforcement : 7.6.1
3 Applicability of boundary element : 10.4.1
4 Muv-Moment Capacity of Web : Annex
5 Additional Compressive Force in BE : 10.4.2
6 Check for BE in tension and compression : 10.4.2.1 and 10.4.3
7 Shear include due to Beam : 7.5
8 Minimum Flexural Strength of Column : 7.2
9 Shear Check at Column Joint : 9.1
10 Length of wall to thickness ratio : 10.1.3
11 Type of wall & Minimum reinforcement : 10.1.4
12 Largest diameter of longitudinal steel bar : 10.1.8
13 Shear reinforcement in RC wall : 10.2.3
14 Special confinement reinforcement in Boundary Element : 10.4.4
15 Minimum vertical reinforcement across horizontal construction joint : 10.7
Sway Calculation (Stability Index)
For Global-X Direction
Level Load Name Storey Height (m) Gravity Load P (kN) Relative Displacements (mm) Storey Shear (kN) Stability Index Sway Condition
A B C D B x C / (A x D)
0 m to 4 m LOAD 1: EQ X+ 4 41384.721 5.964 1586.708 0.039 Non Sway
4 m to 7.5 m LOAD 1: EQ X+ 3.5 36496.211 7.482 1576.153 0.049 Sway
7.5 m to 11 m LOAD 1: EQ X+ 3.5 30902.844 7.607 1537.537 0.044 Sway
11 m to 14.5 m LOAD 1: EQ X+ 3.5 25309.476 7.265 1454.468 0.036 Non Sway
14.5 m to 18 m LOAD 1: EQ X+ 3.5 19716.109 6.561 1310.129 0.028 Non Sway
18 m to 21.5 m LOAD 1: EQ X+ 3.5 14122.742 5.432 1087.698 0.02 Non Sway
21.5 m to 25 m LOAD 1: EQ X+ 3.5 8529.375 3.697 770.357 0.012 Non Sway
25 m to 26.5 m LOAD 1: EQ X+ 1.5 3690.709 0.684 360.781 0.005 Non Sway



For Global-Y Direction
Level Load Name Storey Height (m) Gravity Load P (kN) Relative Displacements (mm) Storey Shear (kN) Stability Index Sway Condition
A B C D B x C / (A x D)
0 m to 4 m LOAD 3: EQ Z+ 4 41384.721 4.748 1586.708 0.031 Non Sway
4 m to 7.5 m LOAD 3: EQ Z+ 3.5 36496.211 6.944 1576.153 0.046 Sway
7.5 m to 11 m LOAD 3: EQ Z+ 3.5 30902.844 7.382 1537.537 0.042 Sway
11 m to 14.5 m LOAD 3: EQ Z+ 3.5 25309.476 7.114 1454.468 0.035 Non Sway
14.5 m to 18 m LOAD 3: EQ Z+ 3.5 19716.109 6.398 1310.129 0.028 Non Sway
18 m to 21.5 m LOAD 3: EQ Z+ 3.5 14122.742 5.238 1087.698 0.019 Non Sway
21.5 m to 25 m LOAD 3: EQ Z+ 3.5 8529.375 3.547 770.357 0.011 Non Sway
25 m to 26.5 m LOAD 3: EQ Z+ 1.5 3690.709 0.782 360.781 0.005 Non Sway




General Data
Column No. : C1
Level : 0 m To 4 m
Frame Type = Non-Ductile
Response Reduction Factor = 3
Design Code = IS 456 : 2000 + IS 13920 : 2016
Grade Of Concrete = M25 N/sqmm
Grade Of Steel (Main) = Fe415 N/sqmm
Grade Of Steel (Shear) = Fe415 N/sqmm
Grade Of Steel - Flexural Design = Fe415 N/sqmm
Grade Of Steel - Shear Design = Fe415 N/sqmm
Column B = 450 mm
Column D = 600 mm
Clear Cover = 50 mm
Clear Floor Height @ B = 3550 mm
Clear Floor Height @ D = 3550 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 : 1.33 <= 4 Hence, Design as Column



Flexural Design (Analysis Forces)
Analysis Reference No. = 1
Critical Analysis Load Combination : 85
Load Combination = [71] : 0.9 (LOAD 5: DEAD) -1.5 (LOAD 2: EQ X-)
Critical Location = Bottom Joint
Pu = 440.5 kN
Mux = -10.21 kNm
Muy = 185.16 kNm
Vux = 60.7 kN
Vuy = 7.72 kN



Effective Length Calculation
Calculation Along Major Axis Of Column
Joint Column Stiffness Beam Sizes Beam Stiffness Beta
Beam 1
(Length x Width x Depth)
Beam 2
(Length x Width x Depth)
Beam 1 Beam 2
N-m x 10^6 mm mm N-m x 10^6 N-m x 10^6
Bottom 202.5 No Beam No Beam - - 1
Top 202.5 No Beam 5000 x 300 x 450 - 45.562 0.905
Sway Condition (as per Stability Index) = Non Sway
Effective Length Factor along Major Axis = 0.96
Calculation Along Minor Axis Of Column
Joint Column Stiffness
Beam Sizes
Beam Stiffness
Beta
Beam 1
(Length x Width x Depth)
Beam 2
(Length x Width x Depth)
Beam 1 Beam 2
N-m x 10^6 mm mm N-m x 10^6 N-m x 10^6
Bottom 113.906 No Beam No Beam - - 1
Top 113.906 4000 x 300 x 450 No Beam 56.953 - 0.811
Sway Condition (as per Stability Index) = Non Sway
Effective Length Factor along Minor axis = 0.93
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 D:
Minimum Eccentricity = Unsupported Length / 500 + D / 30
= 27.1 mm
Minimum Eccentricity > 20 mm
Mminx = Pu x Minimum Eccentricity
= 11.94 kNm
Slenderness Check
Max Slenderness Ratio(L/B) = 7.89
< 60 (Hence Ok)
Column Is Unbraced Along D
Slenderness Check Along D:
Effective Length Factor = 0.96
Slenderness Ratio = Effective Length / D
= 5.68, Column not Slender Along D
Column Is Unbraced Along B
Slenderness Check Along B:
Effective Length Factor = 0.93
Slenderness Ratio = Effective Length / B
= 7.34, Column not Slender Along B



Calculation of Design Moment
Direction Manalysis Mmin (Abs) Mdesign Mslndx (Abs) Mdesign-final
A B C E F
Major Axis - Mux -10.21 11.94 -11.94 0 -11.94
Minor Axis - Muy 185.16 --- 185.16 0 185.16
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 = 440.5 kN
Mux = -11.94 kNm
Muy = 185.16 kNm
Resultant Moment (Combined Action)
Moment Capacity Check
Pt Calculated = 0.72
Reinforcement Provided = 4-T16 + 10-T12
Load Angle = Tan-1(Muy/Mux)
= 86.31 deg
MRes = 185.54 kNm
MCap = 193.11 kNm
Capacity Ratio = MRes/ MCap
= 0.96 <= 1
Shear Calculation Along D Along B
Critical Analysis Load Combination 82 80
Critical Load Combination [68] : 0.9 (LOAD 5: DEAD) +1.5 (LOAD 3: EQ Z+) [66] : 0.9 (LOAD 5: DEAD) +1.5 (LOAD 1: EQ X+)
Design shear force, Vu (kN) -58.3421 60.6985
Pu (kN) 520 417.59
Deff , Beff (mm) 542 392
Design shear stress, Tv Vu / (B x Deff) Vu / (D x Beff)
Tv (N/sqmm) 0.2392 0.2581
Pt (%) 0.358 0.358
Design shear strength, Tc (N/sqmm) 0.4257 0.4257
Shear Strength Enhancement Factor (Compressive Force) 1 + 3 x Pu / ( B x D x Fck)
1.2311 1.1856
Shear Strength Enhancement Factor (Tensile Force) - -
Shear Strength Enhancement Factor (max) 1.5 1.5
Shear Strength Enhancement Factor 1.2311 1.1856
Enhanced shear strength, Tc-e (N/sqmm) 0.524 0.5047
Design shear check Tv < Tc x Enhancement factor Tv < Tc x Enhancement factor
Shear Links Design Shear Links Not Required Shear Links 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
= 4 mm
Criterion for spacing of normal links
Min. Longitudinal Bar dia X 16 = 192 mm
Min. dimension of column = 450 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 : 4 m To 7.5 m
Frame Type = Non-Ductile
Response Reduction Factor = 3
Design Code = IS 456 : 2000 + IS 13920 : 2016
Grade Of Concrete = M25 N/sqmm
Grade Of Steel (Main) = Fe415 N/sqmm
Grade Of Steel (Shear) = Fe415 N/sqmm
Grade Of Steel - Flexural Design = Fe415 N/sqmm
Grade Of Steel - Shear Design = Fe415 N/sqmm
Column B = 450 mm
Column D = 600 mm
Clear Cover = 50 mm
Clear Floor Height @ B = 3050 mm
Clear Floor Height @ D = 3050 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 : 1.33 <= 4 Hence, Design as Column



Flexural Design (Analysis Forces)
Analysis Reference No. = 95
Critical Analysis Load Combination : 57
Load Combination = [43] : 1.5 (LOAD 5: DEAD) +1.5 (LOAD 2: EQ X-)
Critical Location = Bottom Joint
Pu = 1620.74 kN
Mux = -46.11 kNm
Muy = -117.45 kNm
Vux = -64.43 kN
Vuy = 25.25 kN



Effective Length Calculation
Calculation Along Major Axis Of Column
Joint Column Stiffness Beam Sizes Beam Stiffness Beta
Beam 1
(Length x Width x Depth)
Beam 2
(Length x Width x Depth)
Beam 1 Beam 2
N-m x 10^6 mm mm N-m x 10^6 N-m x 10^6
Bottom 231.429 No Beam 5000 x 300 x 450 - 45.562 0.905
Top 231.429 No Beam 5000 x 300 x 450 - 45.562 0.91
Sway Condition (as per Stability Index) = Sway
Effective Length Factor along Major Axis = 3.58
Calculation Along Minor Axis Of Column
Joint Column Stiffness
Beam Sizes
Beam Stiffness
Beta
Beam 1
(Length x Width x Depth)
Beam 2
(Length x Width x Depth)
Beam 1 Beam 2
N-m x 10^6 mm mm N-m x 10^6 N-m x 10^6
Bottom 130.179 4000 x 300 x 450 No Beam 56.953 - 0.811
Top 130.179 4000 x 300 x 450 No Beam 56.953 - 0.821
Sway Condition (as per Stability Index) = Sway
Effective Length Factor along Minor axis = 2.51
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 D:
Minimum Eccentricity = Unsupported Length / 500 + D / 30
= 26.1 mm
Minimum Eccentricity > 20 mm
Mminx = Pu x Minimum Eccentricity
= 42.3 kNm
Slenderness Check
Max Slenderness Ratio(L/B) = 6.78
< 60 (Hence Ok)
Column Is Unbraced Along D
Slenderness Check Along D:
Effective Length Factor = 3.58
Slenderness Ratio = Effective Length / D
= 18.2, Column Slender Along D
Slenderness moment along D = (Pu D/ 2000) (Ley/D)^2
= 161.03 kNm
Column Is Unbraced Along B
Slenderness Check Along B:
Effective Length Factor = 2.51
Slenderness Ratio = Effective Length / B
= 17.01, Column Slender Along B
Slenderness moment along B = (Pu B/ 2000) (Ley/B)^2
= 105.54 kNm
Design slenderness moment along D
Puz = 4017.67 kN
Pd = 1501.31 kN
Reduction factor 'k' for slenderness moment = (Puz - Pu) / (Puz - Pd) < = 1
= 0.95 < = 1, Hence k=0.95
Mslndx = k x 161.03
= 153.38 kNm
Design slenderness moment along B
Puz = 4017.67 kN
Pb = 1405.93 kN
Reduction factor 'k' for slenderness moment = (Puz - Pu) / (Puz - Pb) < = 1
= 0.92 < = 1, Hence k=0.92
Mslndy = k x 105.54
= 96.86 kNm



Calculation of Design Moment
Direction Manalysis Mmin (Abs) Mdesign Mslndx (Abs) Mdesign-final
A B C E F
Major Axis - Mux -46.11 42.3 -46.11 153.38 -199.5
Minor Axis - Muy -117.45 --- -117.45 96.86 -214.31
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 = 1620.74 kN
Mux = -199.5 kNm
Muy = -214.31 kNm
Resultant Moment (Combined Action)
Moment Capacity Check
Pt Calculated = 1.21
Reinforcement Provided = 4-T20 + 10-T16
Load Angle = Tan-1(Muy/Mux)
= 47.05 deg
MRes = 292.8 kNm
MCap = 299.83 kNm
Capacity Ratio = MRes/ MCap
= 0.98 <= 1
Shear Calculation Along D Along B
Critical Analysis Load Combination 62 80
Critical Load Combination [48] : 1.5 (LOAD 5: DEAD) -1.5 (LOAD 3: EQ Z+) [66] : 0.9 (LOAD 5: DEAD) +1.5 (LOAD 1: EQ X+)
Design shear force, Vu (kN) 75.4061 40.5187
Pu (kN) 1509.54 374.04
Deff , Beff (mm) 540 390
Design shear stress, Tv Vu / (B x Deff) Vu / (D x Beff)
Tv (N/sqmm) 0.3103 0.1732
Pt (%) 0.605 0.605
Design shear strength, Tc (N/sqmm) 0.5281 0.5281
Shear Strength Enhancement Factor (Compressive Force) 1 + 3 x Pu / ( B x D x Fck)
1.6709 1.1662
Shear Strength Enhancement Factor (Tensile Force) - -
Shear Strength Enhancement Factor (max) 1.5 1.5
Shear Strength Enhancement Factor 1.5 1.1662
Enhanced shear strength, Tc-e (N/sqmm) 0.7921 0.6159
Design shear check Tv < Tc x Enhancement factor Tv < Tc x Enhancement factor
Shear Links Design Shear Links Not Required Shear Links 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
= 5 mm
Criterion for spacing of normal links
Min. Longitudinal Bar dia X 16 = 256 mm
Min. dimension of column = 450 mm
Max. 300 mm = 300 mm
Provided spacing = 250 mm
Table For Links
Required Provided
Normal Design Shear Design Ductile Design Normal Zone Ductile Zone
Link Dia. 8 --- --- 8 ---
Spacing 250 --- --- 250 ---

General Data
Column No. : C1
Level : 7.5 m To 11 m
Frame Type = Non-Ductile
Response Reduction Factor = 3
Design Code = IS 456 : 2000 + IS 13920 : 2016
Grade Of Concrete = M25 N/sqmm
Grade Of Steel (Main) = Fe415 N/sqmm
Grade Of Steel (Shear) = Fe415 N/sqmm
Grade Of Steel - Flexural Design = Fe415 N/sqmm
Grade Of Steel - Shear Design = Fe415 N/sqmm
Column B = 450 mm
Column D = 600 mm
Clear Cover = 50 mm
Clear Floor Height @ B = 3050 mm
Clear Floor Height @ D = 3050 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 : 1.33 <= 4 Hence, Design as Column



Flexural Design (Analysis Forces)
Analysis Reference No. = 180
Critical Analysis Load Combination : 57
Load Combination = [43] : 1.5 (LOAD 5: DEAD) +1.5 (LOAD 2: EQ X-)
Critical Location = Top Joint
Pu = 1302.59 kN
Mux = 43.34 kNm
Muy = 111.85 kNm
Vux = -62.91 kN
Vuy = 24.64 kN



Effective Length Calculation
Calculation Along Major Axis Of Column
Joint Column Stiffness Beam Sizes Beam Stiffness Beta
Beam 1
(Length x Width x Depth)
Beam 2
(Length x Width x Depth)
Beam 1 Beam 2
N-m x 10^6 mm mm N-m x 10^6 N-m x 10^6
Bottom 231.429 No Beam 5000 x 300 x 450 - 45.562 0.91
Top 231.429 No Beam 5000 x 300 x 450 - 45.562 0.91
Sway Condition (as per Stability Index) = Sway
Effective Length Factor along Major Axis = 3.63
Calculation Along Minor Axis Of Column
Joint Column Stiffness
Beam Sizes
Beam Stiffness
Beta
Beam 1
(Length x Width x Depth)
Beam 2
(Length x Width x Depth)
Beam 1 Beam 2
N-m x 10^6 mm mm N-m x 10^6 N-m x 10^6
Bottom 130.179 4000 x 300 x 450 No Beam 56.953 - 0.821
Top 130.179 4000 x 300 x 450 No Beam 56.953 - 0.821
Sway Condition (as per Stability Index) = Sway
Effective Length Factor along Minor axis = 2.55
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 D:
Minimum Eccentricity = Unsupported Length / 500 + D / 30
= 26.1 mm
Minimum Eccentricity > 20 mm
Mminx = Pu x Minimum Eccentricity
= 34 kNm
Slenderness Check
Max Slenderness Ratio(L/B) = 6.78
< 60 (Hence Ok)
Column Is Unbraced Along D
Slenderness Check Along D:
Effective Length Factor = 3.63
Slenderness Ratio = Effective Length / D
= 18.45, Column Slender Along D
Slenderness moment along D = (Pu D/ 2000) (Ley/D)^2
= 133.06 kNm
Column Is Unbraced Along B
Slenderness Check Along B:
Effective Length Factor = 2.55
Slenderness Ratio = Effective Length / B
= 17.28, Column Slender Along B
Slenderness moment along B = (Pu B/ 2000) (Ley/B)^2
= 87.55 kNm
Design slenderness moment along D
Puz = 3829.18 kN
Pd = 1490.31 kN
Reduction factor 'k' for slenderness moment = (Puz - Pu) / (Puz - Pd) < = 1
= 1.08 > = 1, Hence k=1
Mslndx = k x 133.06
= 133.06 kNm
Design slenderness moment along B
Puz = 3829.18 kN
Pb = 1413.16 kN
Reduction factor 'k' for slenderness moment = (Puz - Pu) / (Puz - Pb) < = 1
= 1.05 < = 1, Hence k=1.05
Mslndy = k x 87.55
= 87.55 kNm



Calculation of Design Moment
Direction Manalysis Mmin (Abs) Mdesign Mslndx (Abs) Mdesign-final
A B C E F
Major Axis - Mux 43.34 34 43.34 133.06 176.4
Minor Axis - Muy 111.85 --- 111.85 87.55 199.4
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 = 1302.59 kN
Mux = 176.4 kNm
Muy = 199.4 kNm
Resultant Moment (Combined Action)
Moment Capacity Check
Pt Calculated = 0.98
Reinforcement Provided = 12-T16 + 2-T12
Load Angle = Tan-1(Muy/Mux)
= 48.5 deg
MRes = 266.22 kNm
MCap = 276.94 kNm
Capacity Ratio = MRes/ MCap
= 0.96 <= 1
Shear Calculation Along D Along B
Critical Analysis Load Combination 86 80
Critical Load Combination [72] : 0.9 (LOAD 5: DEAD) -1.5 (LOAD 3: EQ Z+) [66] : 0.9 (LOAD 5: DEAD) +1.5 (LOAD 1: EQ X+)
Design shear force, Vu (kN) 62.4027 39.9418
Pu (kN) 836.65 332.93
Deff , Beff (mm) 542 392
Design shear stress, Tv Vu / (B x Deff) Vu / (D x Beff)
Tv (N/sqmm) 0.2559 0.1698
Pt (%) 0.489 0.489
Design shear strength, Tc (N/sqmm) 0.4843 0.4843
Shear Strength Enhancement Factor (Compressive Force) 1 + 3 x Pu / ( B x D x Fck)
1.3718 1.148
Shear Strength Enhancement Factor (Tensile Force) - -
Shear Strength Enhancement Factor (max) 1.5 1.5
Shear Strength Enhancement Factor 1.3718 1.148
Enhanced shear strength, Tc-e (N/sqmm) 0.6644 0.556
Design shear check Tv < Tc x Enhancement factor Tv < Tc x Enhancement factor
Shear Links Design Shear Links Not Required Shear Links 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
= 4 mm
Criterion for spacing of normal links
Min. Longitudinal Bar dia X 16 = 192 mm
Min. dimension of column = 450 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 : 11 m To 14.5 m
Frame Type = Non-Ductile
Response Reduction Factor = 3
Design Code = IS 456 : 2000 + IS 13920 : 2016
Grade Of Concrete = M25 N/sqmm
Grade Of Steel (Main) = Fe415 N/sqmm
Grade Of Steel (Shear) = Fe415 N/sqmm
Grade Of Steel - Flexural Design = Fe415 N/sqmm
Grade Of Steel - Shear Design = Fe415 N/sqmm
Column B = 450 mm
Column D = 600 mm
Clear Cover = 50 mm
Clear Floor Height @ B = 3050 mm
Clear Floor Height @ D = 3050 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 : 1.33 <= 4 Hence, Design as Column



Flexural Design (Analysis Forces)
Analysis Reference No. = 265
Critical Analysis Load Combination : 57
Load Combination = [43] : 1.5 (LOAD 5: DEAD) +1.5 (LOAD 2: EQ X-)
Critical Location = Top Joint
Pu = 1019.51 kN
Mux = 44.31 kNm
Muy = 110.1 kNm
Vux = -59.79 kN
Vuy = 25.21 kN



Effective Length Calculation
Calculation Along Major Axis Of Column
Joint Column Stiffness Beam Sizes Beam Stiffness Beta
Beam 1
(Length x Width x Depth)
Beam 2
(Length x Width x Depth)
Beam 1 Beam 2
N-m x 10^6 mm mm N-m x 10^6 N-m x 10^6
Bottom 231.429 No Beam 5000 x 300 x 450 - 45.562 0.91
Top 231.429 No Beam 5000 x 300 x 450 - 45.562 0.91
Sway Condition (as per Stability Index) = Non Sway
Effective Length Factor along Major Axis = 0.93
Calculation Along Minor Axis Of Column
Joint Column Stiffness
Beam Sizes
Beam Stiffness
Beta
Beam 1
(Length x Width x Depth)
Beam 2
(Length x Width x Depth)
Beam 1 Beam 2
N-m x 10^6 mm mm N-m x 10^6 N-m x 10^6
Bottom 130.179 4000 x 300 x 450 No Beam 56.953 - 0.821
Top 130.179 4000 x 300 x 450 No Beam 56.953 - 0.821
Sway Condition (as per Stability Index) = Non Sway
Effective Length Factor along Minor axis = 0.87
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 D:
Minimum Eccentricity = Unsupported Length / 500 + D / 30
= 26.1 mm
Minimum Eccentricity > 20 mm
Mminx = Pu x Minimum Eccentricity
= 26.61 kNm
Slenderness Check
Max Slenderness Ratio(L/B) = 6.78
< 60 (Hence Ok)
Column Is Unbraced Along D
Slenderness Check Along D:
Effective Length Factor = 0.93
Slenderness Ratio = Effective Length / D
= 4.73, Column not Slender Along D
Column Is Unbraced Along B
Slenderness Check Along B:
Effective Length Factor = 0.87
Slenderness Ratio = Effective Length / B
= 5.9, Column not Slender Along B



Calculation of Design Moment
Direction Manalysis Mmin (Abs) Mdesign Mslndx (Abs) Mdesign-final
A B C E F
Major Axis - Mux 44.31 26.61 44.31 0 44.31
Minor Axis - Muy 110.1 --- 110.1 0 110.1
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 = 1019.51 kN
Mux = 44.31 kNm
Muy = 110.1 kNm
Resultant Moment (Combined Action)
Moment Capacity Check
Pt Calculated = 0.42
Reinforcement Provided = 10-T12
Load Angle = Tan-1(Muy/Mux)
= 68.08 deg
MRes = 118.68 kNm
MCap = 197.95 kNm
Capacity Ratio = MRes/ MCap
= 0.6 <= 1
Shear Calculation Along D Along B
Critical Analysis Load Combination 86 84
Critical Load Combination [72] : 0.9 (LOAD 5: DEAD) -1.5 (LOAD 3: EQ Z+) [70] : 0.9 (LOAD 5: DEAD) -1.5 (LOAD 1: EQ X+)
Design shear force, Vu (kN) 59.1315 -53.8068
Pu (kN) 653.79 692.77
Deff , Beff (mm) 544 394
Design shear stress, Tv Vu / (B x Deff) Vu / (D x Beff)
Tv (N/sqmm) 0.2416 0.2276
Pt (%) 0.209 0.209
Design shear strength, Tc (N/sqmm) 0.3376 0.3376
Shear Strength Enhancement Factor (Compressive Force) 1 + 3 x Pu / ( B x D x Fck)
1.2906 1.3079
Shear Strength Enhancement Factor (Tensile Force) - -
Shear Strength Enhancement Factor (max) 1.5 1.5
Shear Strength Enhancement Factor 1.2906 1.3079
Enhanced shear strength, Tc-e (N/sqmm) 0.4356 0.4415
Design shear check Tv < Tc x Enhancement factor Tv < Tc x Enhancement factor
Shear Links Design Shear Links Not Required Shear Links 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 = 450 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 : 14.5 m To 18 m
Frame Type = Non-Ductile
Response Reduction Factor = 3
Design Code = IS 456 : 2000 + IS 13920 : 2016
Grade Of Concrete = M25 N/sqmm
Grade Of Steel (Main) = Fe415 N/sqmm
Grade Of Steel (Shear) = Fe415 N/sqmm
Grade Of Steel - Flexural Design = Fe415 N/sqmm
Grade Of Steel - Shear Design = Fe415 N/sqmm
Column B = 450 mm
Column D = 600 mm
Clear Cover = 50 mm
Clear Floor Height @ B = 3050 mm
Clear Floor Height @ D = 3050 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 : 1.33 <= 4 Hence, Design as Column



Flexural Design (Analysis Forces)
Analysis Reference No. = 350
Critical Analysis Load Combination : 57
Load Combination = [43] : 1.5 (LOAD 5: DEAD) +1.5 (LOAD 2: EQ X-)
Critical Location = Top Joint
Pu = 742.27 kN
Mux = 44.8 kNm
Muy = 105.29 kNm
Vux = -55.07 kN
Vuy = 25.54 kN



Effective Length Calculation
Calculation Along Major Axis Of Column
Joint Column Stiffness Beam Sizes Beam Stiffness Beta
Beam 1
(Length x Width x Depth)
Beam 2
(Length x Width x Depth)
Beam 1 Beam 2
N-m x 10^6 mm mm N-m x 10^6 N-m x 10^6
Bottom 231.429 No Beam 5000 x 300 x 450 - 45.562 0.91
Top 231.429 No Beam 5000 x 300 x 450 - 45.562 0.91
Sway Condition (as per Stability Index) = Non Sway
Effective Length Factor along Major Axis = 0.93
Calculation Along Minor Axis Of Column
Joint Column Stiffness
Beam Sizes
Beam Stiffness
Beta
Beam 1
(Length x Width x Depth)
Beam 2
(Length x Width x Depth)
Beam 1 Beam 2
N-m x 10^6 mm mm N-m x 10^6 N-m x 10^6
Bottom 130.179 4000 x 300 x 450 No Beam 56.953 - 0.821
Top 130.179 4000 x 300 x 450 No Beam 56.953 - 0.821
Sway Condition (as per Stability Index) = Non Sway
Effective Length Factor along Minor axis = 0.87
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 D:
Minimum Eccentricity = Unsupported Length / 500 + D / 30
= 26.1 mm
Minimum Eccentricity > 20 mm
Mminx = Pu x Minimum Eccentricity
= 19.37 kNm
Slenderness Check
Max Slenderness Ratio(L/B) = 6.78
< 60 (Hence Ok)
Column Is Unbraced Along D
Slenderness Check Along D:
Effective Length Factor = 0.93
Slenderness Ratio = Effective Length / D
= 4.73, Column not Slender Along D
Column Is Unbraced Along B
Slenderness Check Along B:
Effective Length Factor = 0.87
Slenderness Ratio = Effective Length / B
= 5.9, Column not Slender Along B



Calculation of Design Moment
Direction Manalysis Mmin (Abs) Mdesign Mslndx (Abs) Mdesign-final
A B C E F
Major Axis - Mux 44.8 19.37 44.8 0 44.8
Minor Axis - Muy 105.29 --- 105.29 0 105.29
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 = 742.27 kN
Mux = 44.8 kNm
Muy = 105.29 kNm
Resultant Moment (Combined Action)
Moment Capacity Check
Pt Calculated = 0.42
Reinforcement Provided = 10-T12
Load Angle = Tan-1(Muy/Mux)
= 66.95 deg
MRes = 114.43 kNm
MCap = 182.75 kNm
Capacity Ratio = MRes/ MCap
= 0.63 <= 1
Shear Calculation Along D Along B
Critical Analysis Load Combination 62 84
Critical Load Combination [48] : 1.5 (LOAD 5: DEAD) -1.5 (LOAD 3: EQ Z+) [70] : 0.9 (LOAD 5: DEAD) -1.5 (LOAD 1: EQ X+)
Design shear force, Vu (kN) 64.5996 -48.957
Pu (kN) 719.12 498.21
Deff , Beff (mm) 544 394
Design shear stress, Tv Vu / (B x Deff) Vu / (D x Beff)
Tv (N/sqmm) 0.2639 0.2071
Pt (%) 0.209 0.209
Design shear strength, Tc (N/sqmm) 0.3376 0.3376
Shear Strength Enhancement Factor (Compressive Force) 1 + 3 x Pu / ( B x D x Fck)
1.3196 1.2214
Shear Strength Enhancement Factor (Tensile Force) - -
Shear Strength Enhancement Factor (max) 1.5 1.5
Shear Strength Enhancement Factor 1.3196 1.2214
Enhanced shear strength, Tc-e (N/sqmm) 0.4454 0.4123
Design shear check Tv < Tc x Enhancement factor Tv < Tc x Enhancement factor
Shear Links Design Shear Links Not Required Shear Links 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 = 450 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 : 18 m To 21.5 m
Frame Type = Non-Ductile
Response Reduction Factor = 3
Design Code = IS 456 : 2000 + IS 13920 : 2016
Grade Of Concrete = M25 N/sqmm
Grade Of Steel (Main) = Fe415 N/sqmm
Grade Of Steel (Shear) = Fe415 N/sqmm
Grade Of Steel - Flexural Design = Fe415 N/sqmm
Grade Of Steel - Shear Design = Fe415 N/sqmm
Column B = 450 mm
Column D = 600 mm
Clear Cover = 50 mm
Clear Floor Height @ B = 3050 mm
Clear Floor Height @ D = 3050 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 : 1.33 <= 4 Hence, Design as Column



Flexural Design (Analysis Forces)
Analysis Reference No. = 435
Critical Analysis Load Combination : 57
Load Combination = [43] : 1.5 (LOAD 5: DEAD) +1.5 (LOAD 2: EQ X-)
Critical Location = Top Joint
Pu = 474.86 kN
Mux = 45.5 kNm
Muy = 97.44 kNm
Vux = -48.1 kN
Vuy = 25.97 kN



Effective Length Calculation
Calculation Along Major Axis Of Column
Joint Column Stiffness Beam Sizes Beam Stiffness Beta
Beam 1
(Length x Width x Depth)
Beam 2
(Length x Width x Depth)
Beam 1 Beam 2
N-m x 10^6 mm mm N-m x 10^6 N-m x 10^6
Bottom 231.429 No Beam 5000 x 300 x 450 - 45.562 0.91
Top 231.429 No Beam 5000 x 300 x 450 - 45.562 0.91
Sway Condition (as per Stability Index) = Non Sway
Effective Length Factor along Major Axis = 0.93
Calculation Along Minor Axis Of Column
Joint Column Stiffness
Beam Sizes
Beam Stiffness
Beta
Beam 1
(Length x Width x Depth)
Beam 2
(Length x Width x Depth)
Beam 1 Beam 2
N-m x 10^6 mm mm N-m x 10^6 N-m x 10^6
Bottom 130.179 4000 x 300 x 450 No Beam 56.953 - 0.821
Top 130.179 4000 x 300 x 450 No Beam 56.953 - 0.821
Sway Condition (as per Stability Index) = Non Sway
Effective Length Factor along Minor axis = 0.87
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 D:
Minimum Eccentricity = Unsupported Length / 500 + D / 30
= 26.1 mm
Minimum Eccentricity > 20 mm
Mminx = Pu x Minimum Eccentricity
= 12.39 kNm
Slenderness Check
Max Slenderness Ratio(L/B) = 6.78
< 60 (Hence Ok)
Column Is Unbraced Along D
Slenderness Check Along D:
Effective Length Factor = 0.93
Slenderness Ratio = Effective Length / D
= 4.73, Column not Slender Along D
Column Is Unbraced Along B
Slenderness Check Along B:
Effective Length Factor = 0.87
Slenderness Ratio = Effective Length / B
= 5.9, Column not Slender Along B



Calculation of Design Moment
Direction Manalysis Mmin (Abs) Mdesign Mslndx (Abs) Mdesign-final
A B C E F
Major Axis - Mux 45.5 12.39 45.5 0 45.5
Minor Axis - Muy 97.44 --- 97.44 0 97.44
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 = 474.86 kN
Mux = 45.5 kNm
Muy = 97.44 kNm
Resultant Moment (Combined Action)
Moment Capacity Check
Pt Calculated = 0.42
Reinforcement Provided = 10-T12
Load Angle = Tan-1(Muy/Mux)
= 64.97 deg
MRes = 107.53 kNm
MCap = 159.47 kNm
Capacity Ratio = MRes/ MCap
= 0.67 <= 1
Shear Calculation Along D Along B
Critical Analysis Load Combination 62 60
Critical Load Combination [48] : 1.5 (LOAD 5: DEAD) -1.5 (LOAD 3: EQ Z+) [46] : 1.5 (LOAD 5: DEAD) -1.5 (LOAD 1: EQ X+)
Design shear force, Vu (kN) 58.1864 -48.1002
Pu (kN) 464.97 474.86
Deff , Beff (mm) 544 394
Design shear stress, Tv Vu / (B x Deff) Vu / (D x Beff)
Tv (N/sqmm) 0.2377 0.2035
Pt (%) 0.209 0.209
Design shear strength, Tc (N/sqmm) 0.3376 0.3376
Shear Strength Enhancement Factor (Compressive Force) 1 + 3 x Pu / ( B x D x Fck)
1.2067 1.211
Shear Strength Enhancement Factor (Tensile Force) - -
Shear Strength Enhancement Factor (max) 1.5 1.5
Shear Strength Enhancement Factor 1.2067 1.211
Enhanced shear strength, Tc-e (N/sqmm) 0.4073 0.4088
Design shear check Tv < Tc x Enhancement factor Tv < Tc x Enhancement factor
Shear Links Design Shear Links Not Required Shear Links 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 = 450 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 : 21.5 m To 25 m
Frame Type = Non-Ductile
Response Reduction Factor = 3
Design Code = IS 456 : 2000 + IS 13920 : 2016
Grade Of Concrete = M25 N/sqmm
Grade Of Steel (Main) = Fe415 N/sqmm
Grade Of Steel (Shear) = Fe415 N/sqmm
Grade Of Steel - Flexural Design = Fe415 N/sqmm
Grade Of Steel - Shear Design = Fe415 N/sqmm
Column B = 450 mm
Column D = 600 mm
Clear Cover = 50 mm
Clear Floor Height @ B = 3050 mm
Clear Floor Height @ D = 3050 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 : 1.33 <= 4 Hence, Design as Column



Flexural Design (Analysis Forces)
Analysis Reference No. = 520
Critical Analysis Load Combination : 59
Load Combination = [45] : 1.5 (LOAD 5: DEAD) +1.5 (LOAD 4: EQ Z-)
Critical Location = Top Joint
Pu = 221.99 kN
Mux = 122.28 kNm
Muy = 23.64 kNm
Vux = -14.52 kN
Vuy = 48.48 kN



Effective Length Calculation
Calculation Along Major Axis Of Column
Joint Column Stiffness Beam Sizes Beam Stiffness Beta
Beam 1
(Length x Width x Depth)
Beam 2
(Length x Width x Depth)
Beam 1 Beam 2
N-m x 10^6 mm mm N-m x 10^6 N-m x 10^6
Bottom 231.429 No Beam 5000 x 300 x 450 - 45.562 0.91
Top 231.429 No Beam 5000 x 300 x 450 - 45.562 0.944
Sway Condition (as per Stability Index) = Non Sway
Effective Length Factor along Major Axis = 0.94
Calculation Along Minor Axis Of Column
Joint Column Stiffness
Beam Sizes
Beam Stiffness
Beta
Beam 1
(Length x Width x Depth)
Beam 2
(Length x Width x Depth)
Beam 1 Beam 2
N-m x 10^6 mm mm N-m x 10^6 N-m x 10^6
Bottom 130.179 4000 x 300 x 450 No Beam 56.953 - 0.821
Top 130.179 4000 x 300 x 450 No Beam 56.953 - 0.884
Sway Condition (as per Stability Index) = Non Sway
Effective Length Factor along Minor axis = 0.89
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 D:
Minimum Eccentricity = Unsupported Length / 500 + D / 30
= 26.1 mm
Minimum Eccentricity > 20 mm
Mminx = Pu x Minimum Eccentricity
= 5.79 kNm
Slenderness Check
Max Slenderness Ratio(L/B) = 6.78
< 60 (Hence Ok)
Column Is Unbraced Along D
Slenderness Check Along D:
Effective Length Factor = 0.94
Slenderness Ratio = Effective Length / D
= 4.78, Column not Slender Along D
Column Is Unbraced Along B
Slenderness Check Along B:
Effective Length Factor = 0.89
Slenderness Ratio = Effective Length / B
= 6.03, Column not Slender Along B



Calculation of Design Moment
Direction Manalysis Mmin (Abs) Mdesign Mslndx (Abs) Mdesign-final
A B C E F
Major Axis - Mux 122.28 5.79 122.28 0 122.28
Minor Axis - Muy 23.64 --- 23.64 0 23.64
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 = 221.99 kN
Mux = 122.28 kNm
Muy = 23.64 kNm
Resultant Moment (Combined Action)
Moment Capacity Check
Pt Calculated = 0.42
Reinforcement Provided = 10-T12
Load Angle = Tan-1(Muy/Mux)
= 10.94 deg
MRes = 124.55 kNm
MCap = 156.17 kNm
Capacity Ratio = MRes/ MCap
= 0.8 <= 1
Shear Calculation Along D Along B
Critical Analysis Load Combination 62 60
Critical Load Combination [48] : 1.5 (LOAD 5: DEAD) -1.5 (LOAD 3: EQ Z+) [46] : 1.5 (LOAD 5: DEAD) -1.5 (LOAD 1: EQ X+)
Design shear force, Vu (kN) 48.478 -38.4055
Pu (kN) 221.99 222.1
Deff , Beff (mm) 544 394
Design shear stress, Tv Vu / (B x Deff) Vu / (D x Beff)
Tv (N/sqmm) 0.198 0.1625
Pt (%) 0.209 0.209
Design shear strength, Tc (N/sqmm) 0.3376 0.3376
Shear Strength Enhancement Factor (Compressive Force) 1 + 3 x Pu / ( B x D x Fck)
1.0987 1.0987
Shear Strength Enhancement Factor (Tensile Force) - -
Shear Strength Enhancement Factor (max) 1.5 1.5
Shear Strength Enhancement Factor 1.0987 1.0987
Enhanced shear strength, Tc-e (N/sqmm) 0.3709 0.3709
Design shear check Tv < Tc x Enhancement factor Tv < Tc x Enhancement factor
Shear Links Design Shear Links Not Required Shear Links 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 = 450 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 : 25 m To 26.5 m
Frame Type = Non-Ductile
Response Reduction Factor = 3
Design Code = IS 456 : 2000 + IS 13920 : 2016
Grade Of Concrete = M25 N/sqmm
Grade Of Steel (Main) = Fe415 N/sqmm
Grade Of Steel (Shear) = Fe415 N/sqmm
Grade Of Steel - Flexural Design = Fe415 N/sqmm
Grade Of Steel - Shear Design = Fe415 N/sqmm
Column B = 450 mm
Column D = 600 mm
Clear Cover = 50 mm
Clear Floor Height @ B = 1050 mm
Clear Floor Height @ D = 1050 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 : 1.33 <= 4 Hence, Design as Column



Flexural Design (Analysis Forces)
Analysis Reference No. = 605
Critical Analysis Load Combination : 59
Load Combination = [45] : 1.5 (LOAD 5: DEAD) +1.5 (LOAD 4: EQ Z-)
Critical Location = Top Joint
Pu = 75.95 kN
Mux = 65.03 kNm
Muy = 23.83 kNm
Vux = -27.06 kN
Vuy = 32.49 kN



Effective Length Calculation
Calculation Along Major Axis Of Column
Joint Column Stiffness Beam Sizes Beam Stiffness Beta
Beam 1
(Length x Width x Depth)
Beam 2
(Length x Width x Depth)
Beam 1 Beam 2
N-m x 10^6 mm mm N-m x 10^6 N-m x 10^6
Bottom 540 No Beam 5000 x 300 x 450 - 45.562 0.944
Top 540 No Beam 5000 x 300 x 450 - 45.562 0.922
Sway Condition (as per Stability Index) = Non Sway
Effective Length Factor along Major Axis = 0.95
Calculation Along Minor Axis Of Column
Joint Column Stiffness
Beam Sizes
Beam Stiffness
Beta
Beam 1
(Length x Width x Depth)
Beam 2
(Length x Width x Depth)
Beam 1 Beam 2
N-m x 10^6 mm mm N-m x 10^6 N-m x 10^6
Bottom 303.75 4000 x 300 x 450 No Beam 56.953 - 0.884
Top 303.75 4000 x 300 x 450 No Beam 56.953 - 0.842
Sway Condition (as per Stability Index) = Non Sway
Effective Length Factor along Minor axis = 0.9
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 D:
Minimum Eccentricity = Unsupported Length / 500 + D / 30
= 22.1 mm
Minimum Eccentricity > 20 mm
Mminx = Pu x Minimum Eccentricity
= 1.68 kNm
Slenderness Check
Max Slenderness Ratio(L/B) = 2.33
< 60 (Hence Ok)
Column Is Unbraced Along D
Slenderness Check Along D:
Effective Length Factor = 0.95
Slenderness Ratio = Effective Length / D
= 1.66, Column not Slender Along D
Column Is Unbraced Along B
Slenderness Check Along B:
Effective Length Factor = 0.9
Slenderness Ratio = Effective Length / B
= 2.1, Column not Slender Along B



Calculation of Design Moment
Direction Manalysis Mmin (Abs) Mdesign Mslndx (Abs) Mdesign-final
A B C E F
Major Axis - Mux 65.03 1.68 65.03 0 65.03
Minor Axis - Muy 23.83 --- 23.83 0 23.83
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 = 75.95 kN
Mux = 65.03 kNm
Muy = 23.83 kNm
Resultant Moment (Combined Action)
Moment Capacity Check
Pt Calculated = 0.42
Reinforcement Provided = 10-T12
Load Angle = Tan-1(Muy/Mux)
= 20.12 deg
MRes = 69.26 kNm
MCap = 123.55 kNm
Capacity Ratio = MRes/ MCap
= 0.56 <= 1
Shear Calculation Along D Along B
Critical Analysis Load Combination 15 15
Critical Load Combination [1] : 1.5 (LOAD 5: DEAD) +1.5 (LOAD 6: LIVE) [1] : 1.5 (LOAD 5: DEAD) +1.5 (LOAD 6: LIVE)
Design shear force, Vu (kN) 45.3561 -32.991
Pu (kN) 78.04 78.04
Deff , Beff (mm) 544 394
Design shear stress, Tv Vu / (B x Deff) Vu / (D x Beff)
Tv (N/sqmm) 0.1853 0.1396
Pt (%) 0.209 0.209
Design shear strength, Tc (N/sqmm) 0.3376 0.3376
Shear Strength Enhancement Factor (Compressive Force) 1 + 3 x Pu / ( B x D x Fck)
1.0347 1.0347
Shear Strength Enhancement Factor (Tensile Force) - -
Shear Strength Enhancement Factor (max) 1.5 1.5
Shear Strength Enhancement Factor 1.0347 1.0347
Enhanced shear strength, Tc-e (N/sqmm) 0.3493 0.3493
Design shear check Tv < Tc x Enhancement factor Tv < Tc x Enhancement factor
Shear Links Design Shear Links Not Required Shear Links 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 = 450 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 --- ---

foundation

Isolated Footing Design (IS 456-2000)

Footing No. Group ID Foundation Geometry
- - Length Width Thickness
1 1 2.20m 2.20m 0.70m

Footing No. Footing Reinforcement Pedestal Reinforcement
- Bottom Reinforcement(Mz) Bottom Reinforcement(Mx) Top Reinforcement(Mz) Top Reinforcement(Mx) Main Steel Trans Steel
1 Ø20 @ 415 mm c/c Ø20 @ 415 mm c/c N/A N/A N/A

Isolated Footing 1


0.7 m0.5 mElevation
1.1 m1.1 m2.2 m2.2 m0.45 m0.6 mXZPlan

Input Values

Footing Geometry

Design Type : Calculate Dimension with user specified minimums as starting value
Minimum Footing Length - X(Fl) : 2000.00 mm
Minimum Footing Width - Z (Fw) : 2000.00 mm
Minimum Footing Thickness(Ft) : 700.00 mm
Eccentricity along X (Oxd) : 0.00 mm
Eccentricity along Z (Ozd) : 0.00 mm

Column Dimensions

Column Shape : Rectangular
Column Length - X (Pl) : 0.45 m
Column Width - Z (Pw) : 0.60 m

Pedestal

Include Pedestal : No
Pedestal Shape : N/A

Design Parameters

Concrete and Rebar Properties

Unit Weight of Concrete : 24.00 kN/m3
Strength of Concrete : 50.00 N/mm2
Yield Strength of Steel : 350.00 N/mm2
Minimum Bar Size : Ø20
Maximum Bar Size : Ø20
Pedestal Minimum Bar Size : Ø8
Pedestal Maximum Bar Size : Ø40
Minimum Bar Spacing : 100.00 mm
Maximum Bar Spacing : 450.00 mm
Pedestal Clear Cover (P, CL) : 50.00 mm
Footing Clear Cover (F, CL) : 50.00 mm

Soil Properties

Unit Weight : 17.60 kN/m3
Base Value of Soil Bearing Capacity : 180.00 kPa
Multiplying factor for soil bearing capacity for ultimate loads : 1.70
Soil Bearing Capacity Type : Gross Bearing Capacity
Soil Surcharge : 0.00 kN/m2
Height of Soil above Footing : 500.00 mm
Type of Depth : Fixed Top
Minimum Percentage of Slab area in Contact for Service Loads : 0.00
Minimum Percentage of Slab area in Contact for Ultimate Loads : 0.00

Sliding and Overturning

Coefficient of Friction : 0.50
Factor of Safety Against Sliding : 1.50
Factor of Safety Against Overturning : 1.50

Global Settings

Top Reinforcement Option : Calculate only when foundation is subjected to uplift forces
Concrete Design Option : Net Pressure(Gross Pressure - Self Weight Pressure)
------------------------------------------------------

Design Calculations

Load Combinations

Load Combination/s- Service Stress Level
Load Combination Number Load Combination Title Load Case Multiplier (a) Soil Bearing Factor (b) Self Weight Factor (c) Code
a - Value specified in the Load Multiplier table
b - Value specified in the Pile/Soil Bearing Capacity Factors table
c - Value specified in the Apply Self Weight and Dead Weight Factor table
5 DEAD 1.00 1.00 1.00 -
6 LIVE 1.00 1.00 1.00 -
Load Combination/s- Strength Level
Load Combination Number Load Combination Title Load Case Multiplier (a) Soil Bearing Factor (b) Self Weight Factor (c) Code
a - Value specified in the Load Multiplier table
b - Value specified in the Pile/Soil Bearing Capacity Factors table
c - Value specified in the Apply Self Weight and Dead Weight Factor table
5 DEAD 1.00 1.00 1.00 -
6 LIVE 1.00 1.00 1.00 -

Applied Loads on Top of Pedestal

Before consideration of self weight and load multiplier table

Moments are About the center of Column / Pedestal (does not include moments caused by lateral loads)
For the loads shown in this table, the sign convention is the same as that for JOINT LOADS in STAAD.Pro when global Y is the vertical axis.

Applied Loads for Column - Service Stress Level
Load Case Fx
(kN)
Fy
(kN)
Downwards is negative Upwards is positive
Fz
(kN)
Mx
(kNm)
Mz
(kNm)
5 -2.94 -661.80 -5.58 -7.69 3.99
6 -0.01 -76.83 0.05 -0.04 0.03
Applied Loads for Column - Strength Level
Load Case Fx
(kN)
Fy
(kN)
Downwards is negative Upwards is positive
Fz
(kN)
Mx
(kNm)
Mz
(kNm)
5 -2.94 -661.80 -5.58 -7.69 3.99
6 -0.01 -76.83 0.05 -0.04 0.03
------------------------------------------------------
Footing Size
Initial Length (Lo) = 2.00 m
Initial Width (Wo) = 2.00 m
Area from initial length and width, Ao
= Lo×Wo = 4.00 m2
Min. area required from bearing pressure, Amin
= Pqmax = 4.23 m2
Note: Amin is an initial estimation.
P = Vertical load from column + selfweight of footing + weight of soil.
qmax = Respective Factored Bearing Capacity.


Final Footing Size
Length (L2) = 2.20 m Governing Load Case : # 5
Width (W2) = 2.20 m Governing Load Case : # 5
Depth (D2) = 0.70 m
Area (A2) = 4.84 m2
Depth is governed by Ultimate Load Case
(Service check is performed with footing thickness requirements from concrete check)
Final Soil Height = 0.50 m
Weight of the footing + pedestal (if any) = 81.31 kN
Weight of the soil above the footing (dry) = 40.22 kN
Uplift force due to buoyancy = 0.00 kN
Effect due to adhesion = 0.00 kN
------------------------------------------------------

Gross Pressures at 4 Corners

Load Case Pressure at top left corner
(kN/m2)
Pressure at top right corner
(kN/m2)
Pressure at bottom right corner
(kN/m2)
Pressure at bottom left corner
(kN/m2)
Area of footing in uplift (Au)
(m2)
Gross Bearing Capacity
(kN/m2)
5 171.7895 164.9758 151.9013 158.7151 0.00 180.0000
5 171.7895 164.9758 151.9013 158.7151 0.00 180.0000
5 171.7895 164.9758 151.9013 158.7151 0.00 180.0000
5 171.7895 164.9758 151.9013 158.7151 0.00 180.0000

If Au is zero, there is no uplift and no pressure adjustment is necessary. Otherwise, to account for uplift, areas of negative pressure will be set to zero and the pressure will be redistributed to remaining corners.

Summary of adjusted Gross Pressures at Four Corners
Load Case Pressure at
top left corner
(kN/m2)
Pressure at
top right corner
(kN/m2)
Pressure at
bottom right corner
(kN/m2)
Pressure at
bottom left corner
(kN/m2)
Gross Bearing Capacity
(kN/m2)
5 171.7895 164.9758 151.9013 158.7151 180.0000
5 171.7895 164.9758 151.9013 158.7151 180.0000
5 171.7895 164.9758 151.9013 158.7151 180.0000
5 171.7895 164.9758 151.9013 158.7151 180.0000
Details of Out-of-Contact Area
(If Any)
Governing load case = N/A
Plan area of footing = 4.84 sq.m
Area not in contact with soil = = 0.00 sq.m
% of total area not in contact = 0.00%
------------------------------------------------------

Stability Check

0.7 m0.5 m.Frictional ForceSliding ForceOTM


- Factor of safety against sliding Factor of safety against overturning
Load Case No. Along X-Direction Along Z-Direction Resultant Required FOS About X-Direction About Z-Direction Required FOS
5 133.09 70.13 62.04 1.50 74.27 142.52 1.50
6 N/A N/A N/A 1.50 N/A N/A 1.50
Critical Load Case And The Governing Factor Of Safety For Overturning and Sliding X Direction
Critical Load Case for Sliding along X-Direction : 5
Governing Disturbing Force : -2.94 kN
Governing Restoring Force : 391.67 kN
Minimum Sliding Ratio for the Critical Load Case : 133.09
Critical Load Case for Overturning About X-Direction : 5
Governing Overturning Moment : -11.60 kNm
Governing Resisting Moment : 861.65 kNm
Minimum Overturning Ratio for the Critical Load Case : 74.27
Critical Load Case And The Governing Factor Of Safety For Overturning and Sliding Z Direction
Critical Load Case for Sliding along Z-Direction : 5
Governing Disturbing Force : -5.58 kN
Governing Restoring Force : 391.67 kN
Minimum Sliding Ratio for the Critical Load Case : 70.13
Critical Load Case for Overturning About Z-Direction : 5
Governing Overturning Moment : 6.05 kNm
Governing Resisting Moment : : 861.65 kNm
Minimum Overturning Ratio for the Critical Load Case : 142.52
Critical Load Case And The Governing Factor Of Safety For Sliding Along Resultant Direction
Critical Load Case for Sliding along Resultant Direction : : 5
Governing Disturbing Force : 6.31 kN
Governing Restoring Force : 391.67 kN
Minimum Sliding Ratio for the Critical Load Case : 62.04
------------------------------------------------------
Top Reinforcement Design Requirement
Top Reinforcement needs to be provided because of resultant negative pressure coming from net pressure calculations for bending.
Ultimate Gross Pressures

The base pressures reported in this table and the area of footing in contact include the effect of buoyancy (if any).

Load Case / Load Combination ID
Pressure at top left corner
(kN/m2)
Pressure at top right corner
(kN/m2)
Pressure at bottom right corner
(kN/m2)
Pressure at bottom left corner
(kN/m2)
Gross Factored Bearing Capacity For Ultimate Load Case
(kN/m2)
Area of footing in Contact with soil (Au)
(m2)
5 171.7895 164.9758 151.9013 158.7151 305.9999 4.84
6 41.0106 40.9704 40.9561 40.9963 305.9999 4.84
Minimum Required Contact Area for Ultimate Loads : 0.00 m2

Actual Area in Contact for all ultimate load cases exceeds the minimum required. Hence Safe

Maximum Corner Pressure from all ultimate load cases is less than the allowable. Hence Safe

Moment Calculation
Check Trial Depth against moment (About Z Axis)
Critical Load Case = #5
Effective Depth = D-(cc+1.5 × db) = 0.62 m
Governing moment (Mu) = = 117.24 kNm
As Per IS 456 2000 ANNEX G G-1.1C
Limiting Factor1 (Kumax) = 700[1100+(0.87 × fy )] = 0.50
Limiting Factor2 (Rumax) = 0.36×fck×kumax×(1-0.42×kumax) = 7093.26 kN/m2
Limiting Moment Of Resistance (Mumax) = Rumax×B×d2 = 5998.52 kNm
Mu <= Mumax hence, safe
Check Trial Depth against moment (About X Axis)
Critical Load Case = #5
Effective Depth = D-(cc+1.5 × db) = 0.62 m
Governing moment (Mu) = = 99.71 kNm
As Per IS 456 2000 ANNEX G G-1.1C
Limiting Factor1 (Kumax) = 700[1100+(0.87×fy )] = 0.50
Limiting Factor2 (Rumax) = 0.36×fck×kumax×(1-0.42×kumax) = 7093.26 kN/m2
Limiting Moment Of Resistance (Mumax) = Rumax × B × d2 = 5998.52 kNm
Mu <= Mumax hence, safe
------------------------------------------------------

One-Way Shear in XY plane

(Shear Plane Parallel to Global X Axis)



1.1 m1.1 m0.18 m0.18 mPlanXZ
Critical Load Case = # 5
Distance of critical section from top left corner along Z, DZ = 0.18 m
Shear Force(S) = 52.84 kN
Shear Stress(Tv) = 38.74 kN/m2
Percentage Of Steel(Pt) = 0.1382
As Per IS 456 2000 Clause 40 Table 19
Shear Strength Of Concrete(Tc) = 300.00 kN/m2
Shear Enhancement Factor (if considered) is applied to (Tc), as per IS456 -2000 Clause No 40.5.1 and Fig 24
Tv< Tc hence, safe

One-Way Shear in YZ plane

(Shear Plane Parallel to Global Z Axis)

1.1 m1.1 m0.255 m0.255 mPlanXZ
Critical Load Case = # 5
Distance of critical section from top left corner along X, DX = 0.25 m
Shear Force(S) = 76.59 kN
Shear Stress(Tv) = 56.15 kN/m2
Percentage Of Steel(Pt) = 0.14
As Per IS 456 2000 Clause 40 Table 19
Shear Strength Of Concrete(Tc) = 300.00 kN/m2
Shear Enhancement Factor (if considered) is applied to (Tc), as per IS456 -2000 Clause No 40.5.1 and Fig 24
Tv< Tc hence, safe

Punching Shear Check

1.1 m1.1 m0.315 mPlanXZ
Critical Load Case = #5
Shear Force(S) = 502.43 kN
Shear Stress(Tv) = 172.62 kN/m2
As Per IS 456 2000 Clause 31.6.3.1
Ks = min⁡[0.5+β,1] = 1.00
Shear Strength(Tc) = 0.25×fck = 1767.77 kN/m2
Ks x Tc = 1767.77 kN/m2
Tv<= Ks x Tc hence, safe
------------------------------------------------------
Reinforcement Calculation
Calculation of Maximum Bar Size
Along X Axis
Bar diameter corresponding to max bar size (db) = 20 mm
As Per IS 456 2000 Clause 26.2.1
Development Length(ld) = db×0.87×fy4×τbd = 0.45 m
Available Development Length(ldb) = (B-b)2-cc = 0.83 m
ldb >=ld hence, safe
Along Z Axis
Bar diameter corresponding to max bar size(db) = 20 mm
As Per IS 456 2000 Clause 26.2.1
Development Length(ld) = db×0.87×fy4×τbd = 0.45 m
Available Development Length(ldb) = (H-h)2-cc = 0.75 m
ldb >=ld hence, safe

Flexure About X-Axis

Design For Bottom Reinforcement Parallel to Z Axis

6 - 20 mmXZ
For moment About X Axis (Mx)
As Per IS 456 2000 Clause 26.5.2.1
Critical Load Case = #5
Minimum Area of Steel (Astmin) = 1848 mm2
Calculated Area of Steel (Ast) = 1848 mm2
Note - "Area of Steel required" reported here is the larger value between the calculated area of steel and minimum steel required as per code stipulations
Provided Area of Steel (Ast,Provided) = 1885 mm2
Ast,Provided >= Astmin Hence OK.

Selected bar Size (db) = Ø20
Minimum spacing allowed (Smin) = 100.00 mm
Selected spacing (S) = 416.00 mm
Smin<= S <= Smax and selected bar size < selected maximum bar size. Hence OK.

Based on spacing reinforcement increment; provided reinforcement is

Ø20 @ 415mm o.c.

Flexure About Z-Axis

Design For Bottom Reinforcement Parallel to X Axis

6 - 20 mmXZ
For moment About Z Axis (Mz)
As Per IS 456 2000 Clause 26.5.2.1
Critical Load Case = #5
Minimum Area of Steel (Astmin) = 1848 mm2
Calculated Area of Steel (Ast) = 1848 mm2
Note - "Area of Steel required" reported here is the larger value between the calculated area of steel and minimum steel required as per code stipulations
Provided Area of Steel (Ast,Provided) = 1885 mm2
Ast,Provided >= Astmin Hence OK.

Selected bar Size (db) = Ø20
Minimum spacing allowed (Smin) = 100.00 mm
Selected spacing (S) = 416.00 mm
Smin<= S <= Smax and selected bar size < selected maximum bar size. Hence OK.

Based on spacing reinforcement increment; provided reinforcement is

Ø20 @ 415mm o.c.
Crack Width Calculation (for Mz)
Modulus of Elasticity of Concrete(Ec) = 35355339.06 kN/m2 Clause No. 6.2.3.1
Modulus of Elasticity of Steel(Es) = 200000000.00 kN/m2 Annexure F
Depth of Neutral Axis(Xu) = 0.33 m Annexure G, Clause No. G-1.1.a
Effective MOI(Ieff) = 26907495888.50 mm4
Average Steel Strain at Considered Level(Ɛm) = 0.00 X 10-5
Distance from Nearest Tension Rod (acr) = 0.22 m
Crack Width (Wcr) = 0.00 mm Annexure F
From IS 456-2000 Clause No. 35.3.2
Section is uncracked.
Crack Width Calculation (for Mx)
Modulus of Elasticity of Concrete(Ec) = 35355339.06 kN/m2 Clause No. 6.2.3.1
Modulus of Elasticity of Steel(Es) = 200000000.00 kN/m2 Annexure F
Depth of Neutral Axis(Xu) = 0.33 m Annexure G, Clause No. G-1.1.a
Effective MOI(Ieff) = 26907495888.50 mm4
Average Steel Strain at Considered Level(Ɛm) = 0.00 X 10-5
Distance from Nearest Tension Rod (acr) = 0.22 m
Crack Width (Wcr) = 0.00 mm Annexure F
From IS 456-2000 Clause No. 35.3.2
Section is uncracked.
------------------------------------------------------
1.1 m1.1 mPlan2.2 m2.2 m0.45 m0.6 mXZ0.7 m0.5 mElevationFoundationPedestalDimensions (m)ReinforcementLBD2.2 m2.2 m0.7 mlbhN/AN/AN/AAstX(T)AstZ(T)AstX(B)AstZ(B)N/AN/A6 - 20 mm6 - 20 mmMain ReinforcementTrans ReinforcementN/AN/A1.1 m1.1 mTOP N/ATOP N/ABOTTOM 6 - 20 mmBOTTOM 6 - 20 mmPlan
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