Serviceability ensures that a beam, slab, or column behaves acceptably under service (un-factored) loads: cracks remain narrow, deflections remain small, and stresses remain in the elastic range. Strength design (USD) prevents collapse; serviceability design keeps the structure usable. The NSCP 2015 / ACI 318 provisions below govern stress checks, cracking, and short- and long-term deflections.
Assumptions for service-load stress investigation (straight-line theory):
Strains vary linearly from the neutral axis (deep beams with $h/L \ge 2/5$ continuous or $4/5$ simple require a non-linear strain distribution).
The stress–strain relationship of concrete is linear within permissible service load stresses.
Concrete resists no tension.
Modular ratio $n = E_s / E_c$ is taken as the nearest whole number (but not less than 6). For deflection computations in lightweight concrete, $n$ is the same as for normal-weight concrete of the same strength.
For doubly-reinforced flexural members, an effective modular ratio of $2E_s/E_c$ is used to transform compression reinforcement; $f'_s$ shall not exceed $f_{sa}$.
Modulus of Elasticity of Concrete
For values of unit weight $w_c$ between 1,440 and 2,560 kg/m³:
where $f_{cm}$ = measured average compressive strength of concrete (MPa). The concrete mixture tested shall be representative of the mixture used in the work.
Cracking Moment, Mcr
The bending moment that first opens a flexural crack is computed from the gross transformed section:
$$M_{cr} = \dfrac{f_r\,I_g}{y_t}$$
where
$I_g$ = moment of inertia of the gross concrete section about the centroidal axis, neglecting reinforcement.
$y_t$ = distance from the centroidal axis of the gross section to the extreme tension fibre.
Calculation of Immediate Deflections
For non-prestressed members, the effective moment of inertia $I_e$ is calculated by the following formula unless obtained by a more comprehensive analysis. $I_e$ shall not be greater than $I_g$:
$I_{cr}$ = moment of inertia of the cracked section transformed to concrete.
$I_e$ = effective moment of inertia for the computation of deflection.
$I_g$ = moment of inertia of the gross concrete section about the centroidal axis, neglecting reinforcement.
$M_{cr}$ = cracking moment $= f_r I_g / y_t$.
$M_a$ = maximum moment in the member at the stage at which deflection is computed.
Typical instantaneous deflection formulas for elastic members (use $I_e$ in place of $I$):
$$\delta_{\text{midspan, simple, UDL}} = \dfrac{5wL^4}{384 E_c I_e}$$
$$\delta_{\text{midspan, simple, P at midspan}} = \dfrac{P L^3}{48 E_c I_e}$$
$$\delta_{\text{cantilever, UDL}} = \dfrac{wL^4}{8 E_c I_e}$$
$$\delta_{\text{cantilever, P at tip}} = \dfrac{P L^3}{3 E_c I_e}$$
Calculation of Time-Dependent Deflections
Unless determined by a more comprehensive analysis, the additional long-term deflection resulting from creep and shrinkage is taken as the immediate deflection caused by the sustained load multiplied by the factor $\lambda_\Delta$:
$$\lambda_\Delta = \dfrac{\xi}{1+50\rho'}$$
where:
$\lambda_\Delta$ = multiplier for additional deflection due to long-term effects.
$\xi$ = time-dependent factor for sustained load.
$\rho' = A'_s/(bd)$ — evaluated at midspan for simple/continuous beams and at the support for cantilevers.
Time-dependent factor $\xi$ for sustained loads:
Sustained Load Duration
Time-Dependent Factor, ξ
3 months
1.0
6 months
1.20
12 months (1 year)
1.40
60 or more months (5 years and up)
2.0
The total long-term deflection is then:
$$\delta_{\text{total}} = \delta_{\text{immediate, all loads}} + \lambda_\Delta\,\delta_{\text{immediate, sustained loads}}$$
Minimum Thickness (Deflections Not Computed) — NSCP Table 409-1
For beams and one-way slabs not supporting or attached to partitions likely to be damaged by large deflections, deflections need not be computed if the member thickness satisfies:
Member
Simply Supported
One-end Continuous
Both-end Continuous
Cantilever
Solid one-way slabs
L/20
L/24
L/28
L/10
Beams or ribbed one-way slabs
L/16
L/18.5
L/21
L/8
Modification factors for the tabulated values:
For structural lightweight concrete with unit weight $w_c$ between 1500 and 2000 kg/m³, multiply by $(1.65 - 0.0003w_c)$ but not less than 1.09.
For $f_y$ other than 420 MPa, multiply by $(0.4 + f_y/700)$.
Factored Load Combinations (Reference)
Although the factored combinations belong to strength design, they are listed here for completeness when checking serviceability against the un-factored counterparts:
$$(1)\;\;U=1.4D$$
$$(2)\;\;U=1.2D+1.6L+0.5(L_r\text{ or }S\text{ or }R)$$
$$(3)\;\;U=1.2D+1.6(L_r\text{ or }S\text{ or }R)+(0.5L\text{ or }0.8W)$$
$$(4)\;\;U=1.2D+1.6W+0.5L+0.5(L_r\text{ or }S\text{ or }R)$$
$$(5)\;\;U=1.2D+1.0E+0.5L+0.2S$$
$$(6)\;\;U=0.9D+(1.6W\text{ or }1.0E)$$
Example: Cracking Moment of a Rectangular Beam
A plain concrete rectangular beam has $b=300\text{ mm}$, $h=600\text{ mm}$, $f'_c=34\text{ MPa}$, normal-weight concrete. Compute the cracking moment $M_{cr}$.
A simply supported beam has a sustained load duration of 5 years and contains compression reinforcement with $\rho' = A'_s/(bd) = 0.012$. Compute the multiplier $\lambda_\Delta$ for additional long-term deflection.