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Beam deflection verification: Bischoff Ie and long-term deflection

This page walks through the complete ACI 318-19 deflection check for test case D1: a 12×20 in simply supported beam spanning 20 ft, with 3-#8 bars, wD = 1.0 klf, wL = 0.8 klf, 5-year duration. The full Bischoff Ie chain is traced from Ec through long-term deflection. Every intermediate value is pinned by a regression test. This is one of 30 cases in the beam verification report.

Case definition

Section12 × 20 in, d = 17.625 in
SpanL = 20 ft, simply supported
Reinforcement3-#8 (As = 2.37 in²)
Materialsf′c = 4,000 psi, Grade 60
LoadswD = 1.0 klf, wL = 0.8 klf
Duration5 years, no compression steel (ρ′ = 0), no sustained live load

Step 1: Material properties

Modulus of elasticity (ACI 318-19 §19.2.2) and modulus of rupture (§19.2.3):

$$E_c = 57\sqrt{f'_c} = 57\sqrt{4{,}000} = 3{,}605\ \text{ksi}$$
$$f_r = 7.5\,\frac{\sqrt{f'_c}}{1{,}000} = 7.5\,\frac{\sqrt{4{,}000}}{1{,}000} = 0.4743\ \text{ksi}$$

Modular ratio n = Es / Ec = 29,000 / 3,605 = 8.044.

Step 2: Gross and cracked moment of inertia

Gross moment of inertia and cracking moment (ACI 318-19 §24.2.3.5):

$$I_g = \frac{bh^3}{12} = \frac{12 \times 20^3}{12} = 8{,}000\ \text{in}^4$$
$$M_{cr} = \frac{f_r \, I_g}{y_t} = \frac{0.4743 \times 8{,}000}{10.0} = 379.47\ \text{kip-in}$$

Cracked neutral axis depth from the transformed-section quadratic, with nAs = 8.044 × 2.37 = 19.064 in²:

$$\frac{b \cdot (kd)^2}{2} = nA_s(d - kd) \quad \Rightarrow \quad kd = 6.062\ \text{in}$$
$$I_{cr} = \frac{b(kd)^3}{3} + nA_s(d - kd)^2 = \frac{12 \times 6.062^3}{3} + 19.064 \times 11.563^2 = 3{,}440.1\ \text{in}^4$$

Step 3: Bischoff effective Ie

ACI 318-19 Table 24.2.3.5 uses the Bischoff formulation instead of the older Branson equation. For moment Ma at the critical section:

$$I_e = \frac{I_{cr}}{1 - \left(\frac{(2/3)\,M_{cr}}{M_a}\right)^2 \left(1 - \frac{I_{cr}}{I_g}\right)}$$

Under dead load only: MD = wDL²/8 = 1.0 × 20²/8 = 50 k-ft = 600 kip-in. Since MD = 600 > Mcr = 379.47, the section is cracked:

$$I_{e,D} = \frac{3{,}440.1}{1 - ((2/3) \times 379.47/600)^2 \times (1 - 3{,}440.1/8{,}000)} = 3{,}828.0\ \text{in}^4$$

Under total load: Mtotal = (wD + wL)L²/8 = 1.8 × 20²/8 = 90 k-ft = 1,080 kip-in:

$$I_{e,total} = \frac{3{,}440.1}{1 - ((2/3) \times 379.47/1{,}080)^2 \times (1 - 3{,}440.1/8{,}000)} = 3{,}551.2\ \text{in}^4$$

Step 4: Immediate and long-term deflection

Immediate deflection under dead load (simply supported, uniform load, wD converted from k/ft to k/in):

$$\delta_D = \frac{5 w_D L^4}{384 E_c I_{e,D}} = \frac{5 \times (1.0/12) \times 240^4}{384 \times 3{,}605 \times 3{,}828.0} = 0.261\ \text{in}$$

Live load deflection δL = 0.225 in (computed from the difference between total-load and dead-load deflections using their respective Ie values).

Long-term multiplier (ACI 318-19 §24.2.4.1) for 5-year duration (ξ = 2.0) with no compression steel (ρ′ = 0):

$$\lambda_\Delta = \frac{\xi}{1 + 50\rho'} = \frac{2.0}{1 + 0} = 2.0$$
$$\delta_{LT} = \delta_D \cdot \lambda_\Delta + \delta_L = 0.261 \times 2.0 + 0.225 = 0.747\ \text{in}$$

Limit checks (Table 24.2.2)

ACI Table 24.2.2 specifies limits for different deflection components: immediate live-load deflection for damage-sensitive limits, and long-term total deflection for partition/attachment limits.

Limit Component Threshold Actual Status
L/180 (flat roofs, no damage) δL 1.333 in 0.225 in PASS
L/360 (floors, no damage) δL 0.667 in 0.225 in PASS
L/480 (floors, brittle partitions) δLT 0.500 in 0.747 in FAIL
L/240 (roofs/floors, nonstructural) δLT 1.000 in 0.747 in PASS

Overall: FAIL (L/480 exceeded). The 12×20 beam with these loads and 5-year creep satisfies immediate live-load limits but exceeds the long-term deflection limit for floors supporting brittle partitions.

Pinned values

These values are locked by regression tests. A drift beyond tolerance fails the build before it can deploy.

Quantity Value ACI reference
Ec3,605 ksiCl 19.2.2
fr0.4743 ksiCl 19.2.3
Ig8,000 in4
Mcr379.47 kip-inCl 24.2.3.5
n8.044
kd6.062 in
Icr3,440.1 in4
Ie (dead)3,828.0 in4Table 24.2.3.5
Ie (total)3,551.2 in4Table 24.2.3.5
δD0.261 in
δL0.225 in
λΔ2.0Cl 24.2.4.1
δLT0.747 in