Simply Supported Beam (Doubly Reinforced Section) Design Steps

Given Data

Step 1: Calculate Effective Depth of Beam (d)

1. Assume nominal clear cover (Table 16, cl. 26.4.2) c = __ mm
2. Assume bar diameter = __ mm (20mm, if not given)
3. Effective cover = clear cover + 0.5 × Bar diameter
Effective depth, d = D - effective cover

Step 2: Calculate Effective Span (leff)

1. leff = Clear span + d
2. leff = Clear span + support width / 2 + support width / 2
Adopt leff = Minimum of (1) & (2)
Note:
  • If only clear span is given or support width not given instead of effective span (leff):
    leff = clear span + d
  • If only c-c span is given instead of eff. span (leff):
    leff = Centre to Centre span

Step 3: Calculate Loads Acting on the Beam

3.1 Dead Load (DL)
Self weight of beam = (b/1000) × (D/1000) × 1 × 25 (Conc. Density, kN/m³) = __ kN/m
+ Other imposed dead load
Total dead load, WDL = __ kN/m
3.2 Live Load (LL)
Total Imposed live load/moving load, WLL = __ kN/m
Factored Design Load
Wu = 1.5 (WDL + WLL) = __ kN/m

Step 4: Calculate Ultimate Forces

4.1 Calculate Ultimate Bending Moment (Mu)
Mu = Wu × leff² / 8 = __ kNm (for UDL)
4.2 Calculate Ultimate Shear Force (Vu)
Vu = Wu × leff / 2
4.3 Calculate Limiting Moment of Resistance of Beam Section (Mu,lim)
Refer Clause G-1-(c), Annexure G, Page 96, IS 456
Mu,lim = 0.36 (xu,max/d) (1 - 0.42 (xu,max/d)) b d² fck
For maximum depth of neutral axis (xu,max) refer Page 70, IS 456
Decision:
  • If Mu,lim > Mu: Then beam section is not sufficient to resist the acting bending moment
  • If Mu,lim < Mu: Design the beam as Doubly Reinforced section

Generally in singly reinforced beam, the size of the beam section will be increased to make Mu,lim > Mu

Step 5: Calculation of Reinforcement

5.1 Compressive Steel (Asc)
Refer Clause G-1.2, Page No. 96, IS 456
Mu - Mu,lim = fsc × Asc × (d - d')
After rearranging: Asc = (Mu - Mu,lim) / [fsc × (d - d')]
Where:
TABLE A: SALIENT POINTS ON THE DESIGN STRESS-STRAIN CURVE FOR COLD-WORKED BARS (SP 16, Clause 1.4)
STRESS LEVEL fy = 415 N/mm² fy = 500 N/mm²
Strain Stress N/mm² Strain Stress N/mm²
0-80 fyd 0.00144 288.7 0.00174 347.8
0-85 fyd 0.00163 306.7 0.00195 369.6
0-90 fyd 0.00192 324.8 0.00226 391.3
0-95 fyd 0.00241 342.8 0.00277 413.0
0-975 fyd 0.00276 351.8 0.00312 423.9
1-0 fyd 0.00380 360.9 0.00417 434.8
NOTE: Linear interpolation may be done for intermediate values.
Provide Compressive Steel (Asc)
Note:
  • Minimum bars = 2 no.
  • Maximum bars = 6 no. in one layer
Calculate Asc,provided = N × Abar
5.2 Tension Steel (Ast)
Refer Clause G-1.2, Page No. 96, IS 456
Ast = Ast1 + Ast2
Where:
Ast1 = [0.36 × fck × b × xu,max] / (0.87 × fy) = __ mm²
Ast2 = Asc × (fsc / (0.87 × fy)) = __ mm²
Check for Minimum Steel (As,min)
Refer Cl. 26.5.1.1 (a)
Ast,min = 0.85 × b × d / fy = __ mm²
Provide Tension Steel
Note:
  • Minimum bars = 2 no.
  • Maximum bar = 6 nos in one layer
Calculate Ast,provided = N × Abar
Provide bars at bottom (tension face of beam)

Step 6: Check for Shear

Calculate Nominal Shear Stress (τv)
Refer Cl. 40.1, IS 456
τv = Vu / (b × d) = __ N/mm²
Get Maximum Shear Stress (τc,max)
Refer Table 20, Page No. 73, IS 456
Table 20: Maximum Shear Stress, τc max, N/mm²
Concrete Grade M 15 M 20 M 25 M 30 M 35 M 40 and above
τc max, N/mm² 2.5 2.8 3.1 3.5 3.7 4.0
(Clauses 40.2.3, 40.2.3.1, 40.5.1 and 41.3.1)
Check τc,max > τv
Clause 40.2.3, IS 456
Calculate Design Shear Strength of Concrete (τc)
Calculate τc from Table No. 19, Page 73, IS 456
→ % steel provided in Tension side (Pt)
Pt = (100 × Ast,provided) / (b × d)
Table 19: Design Shear Strength of Concrete, τc, N/mm²
100As/bd Concrete Grade
M 15 M 20 M 25 M 30 M 35 M 40 & above
≤0.15 0.28 0.28 0.29 0.29 0.29 0.30
0.25 0.35 0.36 0.36 0.37 0.37 0.38
0.50 0.46 0.48 0.49 0.50 0.50 0.51
0.75 0.54 0.56 0.57 0.59 0.59 0.60
1.00 0.60 0.62 0.64 0.66 0.67 0.68
1.25 0.64 0.67 0.70 0.71 0.73 0.74
1.50 0.68 0.72 0.74 0.76 0.78 0.79
1.75 0.71 0.75 0.78 0.80 0.82 0.84
2.00 0.71 0.79 0.82 0.84 0.86 0.88
2.25 0.71 0.81 0.85 0.88 0.90 0.92
2.50 0.71 0.82 0.88 0.91 0.93 0.95
2.75 0.71 0.82 0.90 0.94 0.96 0.98
3.00 and above 0.71 0.82 0.92 0.96 0.99 1.01
(Clauses 40.2.1, 40.2.2, 40.3, 40.4, 40.5.3, 41.3.2, 41.3.3 and 41.4.3)
NOTE: The term As is the area of longitudinal tension reinforcement which continues at least one effective depth beyond the section being considered except at support where the full area of tension reinforcement may be used provided the detailing conforms to 26.2.2 and 26.2.3
Check If τv > τc
If τv > τc, then design shear reinforcement:
Vus = (0.87 × fy × Asv × d) / Sv
Rearrange: Sv = (0.87 × fy × Asv × d) / Vus
Calculate minimum shear spacing for stirrup:
Sv,min = (0.87 × fy × Asv) / (0.4 × b) ②
Maximum stirrup spacing:
Sv = 0.75 × d ③ (Clause 26.5.1.5, Page No. 47, IS 456)
Sv = 300 mm ④ (Clause 26.5.1.5, Page No. 47, IS 456)
Provide stirrup spacing minimum of ①, ②, ③ or ④
If τv ≤ τc, then minimum shear reinforcement must be provided
Sv,min = (0.87 × fy × Asv) / (0.4 × b) ②
Maximum stirrup spacing:
Sv = 0.75 × d ③ (Clause 26.5.1.5, Page No. 47, IS 456)
Sv = 300 mm ④ (Clause 26.5.1.5, Page No. 47, IS 456)
Provide stirrup spacing minimum of ②, ③ or ④
Final stirrup spacing = the smallest value among Sv(min), 0.75d, and 300 mm