ACI 350.3-06

Seismic loads, rectangular tank

Seismic design forces and overturning moments for a rectangular liquid-containing tank. Calculate seismic design forces for rectangular liquid-containing tanks per ACI 350.3-06. The calculator separates the liquid mass into impulsive and convective components, determines corresponding seismic coefficients, and computes wall pressures and base shear. Input tank geometry, liquid properties, and site seismic parameters for a complete load determination.

Given

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changed from the declared value \(L\) \(\mathrm{m}\) 1-100
changed from the declared value \(h_{\mathrm{wall}}\) \(\mathrm{m}\) 1-40
changed from the declared value \(h_{\mathrm{fluid}}\) \(\mathrm{m}\) 0.5-40
changed from the declared value \(h_{\mathrm{eg}}\) \(\mathrm{m}\) 0-40
changed from the declared value \(t_{\mathrm{wall}}\) \(\mathrm{mm}\) 100-2,000
changed from the declared value \(t_{\mathrm{roof}}\) \(\mathrm{mm}\) 0-2,000
changed from the declared value \(t_{\mathrm{bottom}}\) \(\mathrm{mm}\) 0-2,000
changed from the declared value \(\gamma_{\mathrm{fluid}}\) \(\mathrm{kN/m³}\) 1-30
changed from the declared value \(\gamma_{\mathrm{conc}}\) \(\mathrm{kN/m³}\) 15-30
changed from the declared value \(g\) \(\mathrm{m} \cdot \mathrm{s}^{-2}\) 9-10
changed from the declared value \(I\) 1-1.5
changed from the declared value \(S_{s}\) 0-3
changed from the declared value \(S_{1}\) 0-3
changed from the declared value \(F_{a}\) 0.5-3
changed from the declared value \(F_{v}\) 0.5-3
changed from the declared value \(R_{\mathrm{wi}}\) 1-4
changed from the declared value \(P_{\mathrm{eg}}\) \(\mathrm{kN}\) 0-10,000
changed from the declared value \(W_{r}\) \(\mathrm{kN}\) 0-10,000
L = 18 m twall = 650 mm hfluid = 9.15 m hwall = 10.35 m Direction of shaking
The tank in section, with the geometry the inputs name.
hfreeboard = 1.2 m qhy = 89.8 kPa piy = 67.5 kPa pwy = 8.6 kPa pcy = 3.2 kPa
Section 9.5 wall pressures, each drawn straight between its traced endpoints.

Title block

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Checks

Check D/C Utilisation Result
Freeboard adequate\(\htmlClass{sym-h_freeboard}{h_{\mathrm{freeboard}}} \geq 0\ \mathrm{m} \quad \Rightarrow \quad \htmlClass{sym-h_freeboard}{1.2\ \mathrm{m}} \geq 0\ \mathrm{m}\) 0.00 PASS

Results

Quantity Description Value Unit
\(\htmlClass{sym-V}{V}\) Total design base shear 894.9 \(\mathrm{kN}\)
\(\htmlClass{sym-V_t}{V_{t}}\) Fluid design shear at the top of the foundation 715.5 \(\mathrm{kN}\)
\(\htmlClass{sym-M_s}{M_{s}}\) Overturning moment at the base of the shell 3.44 \(\mathrm{MN} \cdot \mathrm{m}\)
\(\htmlClass{sym-M_s_prime}{{M'}_{s}}\) Overturning moment including base pressure 6.099 \(\mathrm{MN} \cdot \mathrm{m}\)
\(\htmlClass{sym-T_c}{T_{c}}\) Convective (sloshing) period 4.992 \(\mathrm{s}\)
\(\htmlClass{sym-h_freeboard}{h_{\mathrm{freeboard}}}\) Freeboard above the fluid surface 1.2 \(\mathrm{m}\)

Derivation

S.1 \[\begin{aligned} \htmlClass{sym-rho_c}{\rho_{c}} &= \frac{\htmlClass{sym-gamma_conc}{\gamma_{\mathrm{conc}}}}{\htmlClass{sym-g}{g}} \\ &= \frac{\htmlClass{sym-gamma_conc}{23.56\ \mathrm{kN/m³}}}{\htmlClass{sym-g}{9.78\ \mathrm{m} \cdot \mathrm{s}^{-2}}} \\ &= 2409\ \mathrm{kg} \cdot \mathrm{m}^{-3} \end{aligned}\]
S.2 \[\begin{aligned} \htmlClass{sym-rho_L}{\rho_{L}} &= \frac{\htmlClass{sym-gamma_fluid}{\gamma_{\mathrm{fluid}}}}{\htmlClass{sym-g}{g}} \\ &= \frac{\htmlClass{sym-gamma_fluid}{9.81\ \mathrm{kN/m³}}}{\htmlClass{sym-g}{9.78\ \mathrm{m} \cdot \mathrm{s}^{-2}}} \\ &= 1003\ \mathrm{kg} \cdot \mathrm{m}^{-3} \end{aligned}\]
S.3 \[\begin{aligned} \htmlClass{sym-B}{B} &= 1\ \mathrm{m} \end{aligned}\]
S.4 \[\begin{aligned} \htmlClass{sym-W_fluid}{W_{\mathrm{fluid}}} &= \htmlClass{sym-L}{L} \cdot \htmlClass{sym-B}{B} \cdot \htmlClass{sym-h_fluid}{h_{\mathrm{fluid}}} \cdot \htmlClass{sym-gamma_fluid}{\gamma_{\mathrm{fluid}}} \\ &= \htmlClass{sym-L}{18\ \mathrm{m}} \cdot \htmlClass{sym-B}{1\ \mathrm{m}} \cdot \htmlClass{sym-h_fluid}{9.15\ \mathrm{m}} \cdot \htmlClass{sym-gamma_fluid}{9.81\ \mathrm{kN/m³}} \\ &= 1.616\ \mathrm{MN} \end{aligned}\]
S.5 \[\begin{aligned} \htmlClass{sym-h_freeboard}{h_{\mathrm{freeboard}}} &= \htmlClass{sym-h_wall}{h_{\mathrm{wall}}} - \htmlClass{sym-h_fluid}{h_{\mathrm{fluid}}} \\ &= \htmlClass{sym-h_wall}{10.35\ \mathrm{m}} - \htmlClass{sym-h_fluid}{9.15\ \mathrm{m}} \\ &= 1.2\ \mathrm{m} \end{aligned}\]
S.6 \[\begin{aligned} \htmlClass{sym-W_i}{W_{i}} &= \frac{\tanh\left(0.866 \cdot \frac{\htmlClass{sym-L}{L}}{\htmlClass{sym-h_fluid}{h_{\mathrm{fluid}}}}\right)}{0.866 \cdot \frac{\htmlClass{sym-L}{L}}{\htmlClass{sym-h_fluid}{h_{\mathrm{fluid}}}}} \cdot \htmlClass{sym-W_fluid}{W_{\mathrm{fluid}}} \\ &= \frac{\tanh\left(0.866 \cdot \frac{\htmlClass{sym-L}{18\ \mathrm{m}}}{\htmlClass{sym-h_fluid}{9.15\ \mathrm{m}}}\right)}{0.866 \cdot \frac{\htmlClass{sym-L}{18\ \mathrm{m}}}{\htmlClass{sym-h_fluid}{9.15\ \mathrm{m}}}} \cdot \htmlClass{sym-W_fluid}{1.616\ \mathrm{MN}} \\ &= 887.6\ \mathrm{kN} \end{aligned}\]
S.7 \[\begin{aligned} \htmlClass{sym-W_c}{W_{c}} &= 0.264 \cdot \frac{\htmlClass{sym-L}{L}}{\htmlClass{sym-h_fluid}{h_{\mathrm{fluid}}}} \cdot \tanh\left(\frac{3.16 \cdot \htmlClass{sym-h_fluid}{h_{\mathrm{fluid}}}}{\htmlClass{sym-L}{L}}\right) \cdot \htmlClass{sym-W_fluid}{W_{\mathrm{fluid}}} \\ &= 0.264 \cdot \frac{\htmlClass{sym-L}{18\ \mathrm{m}}}{\htmlClass{sym-h_fluid}{9.15\ \mathrm{m}}} \cdot \tanh\left(\frac{3.16 \cdot \htmlClass{sym-h_fluid}{9.15\ \mathrm{m}}}{\htmlClass{sym-L}{18\ \mathrm{m}}}\right) \cdot \htmlClass{sym-W_fluid}{1.616\ \mathrm{MN}} \\ &= 774.2\ \mathrm{kN} \end{aligned}\]
S.8 \[\begin{aligned} \htmlClass{sym-W_walls}{W_{\mathrm{walls}}} &= \htmlClass{sym-gamma_conc}{\gamma_{\mathrm{conc}}} \cdot 2 \cdot \htmlClass{sym-t_wall}{t_{\mathrm{wall}}} \cdot \htmlClass{sym-h_wall}{h_{\mathrm{wall}}} \cdot \htmlClass{sym-B}{B} \\ &= \htmlClass{sym-gamma_conc}{23.56\ \mathrm{kN/m³}} \cdot 2 \cdot \htmlClass{sym-t_wall}{650\ \mathrm{mm}} \cdot \htmlClass{sym-h_wall}{10.35\ \mathrm{m}} \cdot \htmlClass{sym-B}{1\ \mathrm{m}} \\ &= 317\ \mathrm{kN} \end{aligned}\]
S.9 \[\begin{aligned} \htmlClass{sym-W_bottom}{W_{\mathrm{bottom}}} &= \htmlClass{sym-L}{L} \cdot \htmlClass{sym-B}{B} \cdot \htmlClass{sym-gamma_conc}{\gamma_{\mathrm{conc}}} \cdot \htmlClass{sym-t_bottom}{t_{\mathrm{bottom}}} \\ &= \htmlClass{sym-L}{18\ \mathrm{m}} \cdot \htmlClass{sym-B}{1\ \mathrm{m}} \cdot \htmlClass{sym-gamma_conc}{23.56\ \mathrm{kN/m³}} \cdot \htmlClass{sym-t_bottom}{0\ \mathrm{mm}} \\ &= 0\ \mathrm{N} \end{aligned}\]
S.10 \[\begin{aligned} \htmlClass{sym-S_ds}{S_{\mathrm{ds}}} &= \htmlClass{sym-S_s}{S_{s}} \cdot \htmlClass{sym-F_a}{F_{a}} \\ &= \htmlClass{sym-S_s}{1.06} \cdot \htmlClass{sym-F_a}{1} \\ &= 1.06 \end{aligned}\]
S.11 \[\begin{aligned} \htmlClass{sym-S_d1}{S_{d1}} &= \htmlClass{sym-S_1}{S_{1}} \cdot \htmlClass{sym-F_v}{F_{v}} \\ &= \htmlClass{sym-S_1}{0.5} \cdot \htmlClass{sym-F_v}{1} \\ &= 0.5 \end{aligned}\]
S.12 \[\begin{aligned} \htmlClass{sym-T_s}{T_{s}} &= \frac{\htmlClass{sym-S_d1}{S_{d1}}}{\htmlClass{sym-S_ds}{S_{\mathrm{ds}}}} \\ &= \frac{\htmlClass{sym-S_d1}{0.5}}{\htmlClass{sym-S_ds}{1.06}} \\ &= 0.4717 \end{aligned}\]
S.13 \[\begin{aligned} \htmlClass{sym-C_t}{C_{t}} &= 0.4 \cdot \htmlClass{sym-S_ds}{S_{\mathrm{ds}}} \\ &= 0.4 \cdot \htmlClass{sym-S_ds}{1.06} \\ &= 0.424 \end{aligned}\]
S.14 \[\begin{aligned} \htmlClass{sym-m_w}{m_{w}} &= \htmlClass{sym-h_wall}{h_{\mathrm{wall}}} \cdot \htmlClass{sym-t_wall}{t_{\mathrm{wall}}} \cdot \htmlClass{sym-rho_c}{\rho_{c}} \\ &= \htmlClass{sym-h_wall}{10.35\ \mathrm{m}} \cdot \htmlClass{sym-t_wall}{650\ \mathrm{mm}} \cdot \htmlClass{sym-rho_c}{2409\ \mathrm{kg} \cdot \mathrm{m}^{-3}} \\ &= 16206\ \mathrm{kg} \cdot \mathrm{m}^{-1} \end{aligned}\]
S.15 \[\begin{aligned} \htmlClass{sym-m_i}{m_{i}} &= \frac{\frac{\htmlClass{sym-W_i}{W_{i}}}{\htmlClass{sym-W_fluid}{W_{\mathrm{fluid}}}} \cdot \htmlClass{sym-L}{L}}{2} \cdot \htmlClass{sym-h_wall}{h_{\mathrm{wall}}} \cdot \htmlClass{sym-rho_L}{\rho_{L}} \\ &= \frac{\frac{\htmlClass{sym-W_i}{887.6\ \mathrm{kN}}}{\htmlClass{sym-W_fluid}{1.616\ \mathrm{MN}}} \cdot \htmlClass{sym-L}{18\ \mathrm{m}}}{2} \cdot \htmlClass{sym-h_wall}{10.35\ \mathrm{m}} \cdot \htmlClass{sym-rho_L}{1003\ \mathrm{kg} \cdot \mathrm{m}^{-3}} \\ &= 51326\ \mathrm{kg} \cdot \mathrm{m}^{-1} \end{aligned}\]
S.16 \[\begin{aligned} \htmlClass{sym-T_c}{T_{c}} &= 2 \cdot \pi \cdot \sqrt{\frac{\htmlClass{sym-L}{L}}{3.16 \cdot \htmlClass{sym-g}{g} \cdot \tanh\left(\frac{3.16 \cdot \htmlClass{sym-h_fluid}{h_{\mathrm{fluid}}}}{\htmlClass{sym-L}{L}}\right)}} \\ &= 2 \cdot \pi \cdot \sqrt{\frac{\htmlClass{sym-L}{18\ \mathrm{m}}}{3.16 \cdot \htmlClass{sym-g}{9.78\ \mathrm{m} \cdot \mathrm{s}^{-2}} \cdot \tanh\left(\frac{3.16 \cdot \htmlClass{sym-h_fluid}{9.15\ \mathrm{m}}}{\htmlClass{sym-L}{18\ \mathrm{m}}}\right)}} \\ &= 4.992\ \mathrm{s} \end{aligned}\]

Branch: \(T_{c} \leq \frac{1.6\ \mathrm{s}}{T_{s}}\) did not hold

S.17 \[\begin{aligned} \htmlClass{sym-C_c}{C_{c}} &= \frac{2.4 \cdot \htmlClass{sym-S_ds}{S_{\mathrm{ds}}} \cdot 1\ \mathrm{s}^{2}}{\htmlClass{sym-T_c}{T_{c}}^{2}} \\ &= \frac{2.4 \cdot \htmlClass{sym-S_ds}{1.06} \cdot 1\ \mathrm{s}^{2}}{\left(\htmlClass{sym-T_c}{4.992\ \mathrm{s}}\right)^{2}} \\ &= 0.1021 \end{aligned}\]
S.18 \[\begin{aligned} \htmlClass{sym-epsilon}{\epsilon} &= \min\left(0.0151 \cdot \left(\frac{\htmlClass{sym-L}{L}}{\htmlClass{sym-h_fluid}{h_{\mathrm{fluid}}}}\right)^{2} - 0.1908 \cdot \frac{\htmlClass{sym-L}{L}}{\htmlClass{sym-h_fluid}{h_{\mathrm{fluid}}}} + 1.021, 1\right) \\ &= \min\left(0.0151 \cdot \left(\frac{\htmlClass{sym-L}{18\ \mathrm{m}}}{\htmlClass{sym-h_fluid}{9.15\ \mathrm{m}}}\right)^{2} - 0.1908 \cdot \frac{\htmlClass{sym-L}{18\ \mathrm{m}}}{\htmlClass{sym-h_fluid}{9.15\ \mathrm{m}}} + 1.021, 1\right) \\ &= 0.7041 \end{aligned}\]

Branch: \(\frac{L}{h_{\mathrm{fluid}}} < 0.75\) did not hold

S.19 \[\begin{aligned} \htmlClass{sym-h_i_prime}{{h'}_{i}} &= \left(\frac{\frac{0.866 \cdot \htmlClass{sym-L}{L}}{\htmlClass{sym-h_fluid}{h_{\mathrm{fluid}}}}}{2 \cdot \tanh\left(\frac{0.866 \cdot \htmlClass{sym-L}{L}}{\htmlClass{sym-h_fluid}{h_{\mathrm{fluid}}}}\right)} - \frac{1}{8}\right) \cdot \htmlClass{sym-h_fluid}{h_{\mathrm{fluid}}} \\ &= \left(\frac{\frac{0.866 \cdot \htmlClass{sym-L}{18\ \mathrm{m}}}{\htmlClass{sym-h_fluid}{9.15\ \mathrm{m}}}}{2 \cdot \tanh\left(\frac{0.866 \cdot \htmlClass{sym-L}{18\ \mathrm{m}}}{\htmlClass{sym-h_fluid}{9.15\ \mathrm{m}}}\right)} - \frac{1}{8}\right) \cdot \htmlClass{sym-h_fluid}{9.15\ \mathrm{m}} \\ &= 7.184\ \mathrm{m} \end{aligned}\]
S.20 \[\begin{aligned} \htmlClass{sym-h_c_prime}{{h'}_{c}} &= \left(1 - \frac{\cosh\left(\frac{3.16 \cdot \htmlClass{sym-h_fluid}{h_{\mathrm{fluid}}}}{\htmlClass{sym-L}{L}}\right) - 2.01}{\frac{3.16 \cdot \htmlClass{sym-h_fluid}{h_{\mathrm{fluid}}}}{\htmlClass{sym-L}{L}} \cdot \sinh\left(\frac{3.16 \cdot \htmlClass{sym-h_fluid}{h_{\mathrm{fluid}}}}{\htmlClass{sym-L}{L}}\right)}\right) \cdot \htmlClass{sym-h_fluid}{h_{\mathrm{fluid}}} \\ &= \left(1 - \frac{\cosh\left(\frac{3.16 \cdot \htmlClass{sym-h_fluid}{9.15\ \mathrm{m}}}{\htmlClass{sym-L}{18\ \mathrm{m}}}\right) - 2.01}{\frac{3.16 \cdot \htmlClass{sym-h_fluid}{9.15\ \mathrm{m}}}{\htmlClass{sym-L}{18\ \mathrm{m}}} \cdot \sinh\left(\frac{3.16 \cdot \htmlClass{sym-h_fluid}{9.15\ \mathrm{m}}}{\htmlClass{sym-L}{18\ \mathrm{m}}}\right)}\right) \cdot \htmlClass{sym-h_fluid}{9.15\ \mathrm{m}} \\ &= 7.763\ \mathrm{m} \end{aligned}\]
S.21 \[\begin{aligned} \htmlClass{sym-H_w}{H_{w}} &= \frac{\htmlClass{sym-h_wall}{h_{\mathrm{wall}}}}{2} \\ &= \frac{\htmlClass{sym-h_wall}{10.35\ \mathrm{m}}}{2} \\ &= 5.175\ \mathrm{m} \end{aligned}\]
S.22 \[\begin{aligned} \htmlClass{sym-h_roof}{h_{\mathrm{roof}}} &= \htmlClass{sym-h_wall}{h_{\mathrm{wall}}} + \frac{\htmlClass{sym-t_roof}{t_{\mathrm{roof}}}}{2} \\ &= \htmlClass{sym-h_wall}{10.35\ \mathrm{m}} + \frac{\htmlClass{sym-t_roof}{0\ \mathrm{mm}}}{2} \\ &= 10.35\ \mathrm{m} \end{aligned}\]

Branch: \(\frac{L}{h_{\mathrm{fluid}}} < 1.333\) did not hold

S.23 \[\begin{aligned} \htmlClass{sym-h_i}{h_{i}} &= 0.375 \cdot \htmlClass{sym-h_fluid}{h_{\mathrm{fluid}}} \\ &= 0.375 \cdot \htmlClass{sym-h_fluid}{9.15\ \mathrm{m}} \\ &= 3.431\ \mathrm{m} \end{aligned}\]
S.24 \[\begin{aligned} \htmlClass{sym-h_c}{h_{c}} &= \left(1 - \frac{\cosh\left(\frac{3.16 \cdot \htmlClass{sym-h_fluid}{h_{\mathrm{fluid}}}}{\htmlClass{sym-L}{L}}\right) - 1}{\frac{3.16 \cdot \htmlClass{sym-h_fluid}{h_{\mathrm{fluid}}}}{\htmlClass{sym-L}{L}} \cdot \sinh\left(\frac{3.16 \cdot \htmlClass{sym-h_fluid}{h_{\mathrm{fluid}}}}{\htmlClass{sym-L}{L}}\right)}\right) \cdot \htmlClass{sym-h_fluid}{h_{\mathrm{fluid}}} \\ &= \left(1 - \frac{\cosh\left(\frac{3.16 \cdot \htmlClass{sym-h_fluid}{9.15\ \mathrm{m}}}{\htmlClass{sym-L}{18\ \mathrm{m}}}\right) - 1}{\frac{3.16 \cdot \htmlClass{sym-h_fluid}{9.15\ \mathrm{m}}}{\htmlClass{sym-L}{18\ \mathrm{m}}} \cdot \sinh\left(\frac{3.16 \cdot \htmlClass{sym-h_fluid}{9.15\ \mathrm{m}}}{\htmlClass{sym-L}{18\ \mathrm{m}}}\right)}\right) \cdot \htmlClass{sym-h_fluid}{9.15\ \mathrm{m}} \\ &= 5.357\ \mathrm{m} \end{aligned}\]
S.25 \[\begin{aligned} \htmlClass{sym-P_w}{P_{w}} &= \frac{\htmlClass{sym-I}{I} \cdot \htmlClass{sym-S_ds}{S_{\mathrm{ds}}} \cdot \htmlClass{sym-epsilon}{\epsilon} \cdot \htmlClass{sym-W_walls}{W_{\mathrm{walls}}}}{\htmlClass{sym-R_wi}{R_{\mathrm{wi}}}} \\ &= \frac{\htmlClass{sym-I}{1.5} \cdot \htmlClass{sym-S_ds}{1.06} \cdot \htmlClass{sym-epsilon}{0.7041} \cdot \htmlClass{sym-W_walls}{317\ \mathrm{kN}}}{\htmlClass{sym-R_wi}{2}} \\ &= 177.4\ \mathrm{kN} \end{aligned}\]
S.26 \[\begin{aligned} \htmlClass{sym-P_r}{P_{r}} &= \frac{\htmlClass{sym-I}{I} \cdot \htmlClass{sym-S_ds}{S_{\mathrm{ds}}} \cdot \htmlClass{sym-W_r}{W_{r}}}{\htmlClass{sym-R_wi}{R_{\mathrm{wi}}}} \\ &= \frac{\htmlClass{sym-I}{1.5} \cdot \htmlClass{sym-S_ds}{1.06} \cdot \htmlClass{sym-W_r}{5\ \mathrm{kN}}}{\htmlClass{sym-R_wi}{2}} \\ &= 3.975\ \mathrm{kN} \end{aligned}\]
S.27 \[\begin{aligned} \htmlClass{sym-P_i}{P_{i}} &= \frac{\htmlClass{sym-I}{I} \cdot \htmlClass{sym-S_ds}{S_{\mathrm{ds}}} \cdot \htmlClass{sym-W_i}{W_{i}}}{\htmlClass{sym-R_wi}{R_{\mathrm{wi}}}} \\ &= \frac{\htmlClass{sym-I}{1.5} \cdot \htmlClass{sym-S_ds}{1.06} \cdot \htmlClass{sym-W_i}{887.6\ \mathrm{kN}}}{\htmlClass{sym-R_wi}{2}} \\ &= 705.6\ \mathrm{kN} \end{aligned}\]
S.28 \[\begin{aligned} \htmlClass{sym-P_c}{P_{c}} &= \htmlClass{sym-C_c}{C_{c}} \cdot \htmlClass{sym-I}{I} \cdot \htmlClass{sym-W_c}{W_{c}} \\ &= \htmlClass{sym-C_c}{0.1021} \cdot \htmlClass{sym-I}{1.5} \cdot \htmlClass{sym-W_c}{774.2\ \mathrm{kN}} \\ &= 118.5\ \mathrm{kN} \end{aligned}\]
S.29 \[\begin{aligned} \htmlClass{sym-V_t}{V_{t}} &= \sqrt{\htmlClass{sym-P_c}{P_{c}}^{2} + \htmlClass{sym-P_i}{P_{i}}^{2}} \\ &= \sqrt{\left(\htmlClass{sym-P_c}{118.5\ \mathrm{kN}}\right)^{2} + \left(\htmlClass{sym-P_i}{705.6\ \mathrm{kN}}\right)^{2}} \\ &= 715.5\ \mathrm{kN} \end{aligned}\]
S.30 \[\begin{aligned} \htmlClass{sym-V}{V} &= \sqrt{\left(\htmlClass{sym-P_i}{P_{i}} + \htmlClass{sym-P_w}{P_{w}} + \htmlClass{sym-P_r}{P_{r}}\right)^{2} + \htmlClass{sym-P_c}{P_{c}}^{2} + \htmlClass{sym-P_eg}{P_{\mathrm{eg}}}^{2}} \\ &= \sqrt{\left(\htmlClass{sym-P_i}{705.6\ \mathrm{kN}} + \htmlClass{sym-P_w}{177.4\ \mathrm{kN}} + \htmlClass{sym-P_r}{3.975\ \mathrm{kN}}\right)^{2} + \left(\htmlClass{sym-P_c}{118.5\ \mathrm{kN}}\right)^{2} + \left(\htmlClass{sym-P_eg}{0\ \mathrm{kN}}\right)^{2}} \\ &= 894.9\ \mathrm{kN} \end{aligned}\]
S.31 \[\begin{aligned} \htmlClass{sym-M_w}{M_{w}} &= \htmlClass{sym-P_w}{P_{w}} \cdot \htmlClass{sym-H_w}{H_{w}} \\ &= \htmlClass{sym-P_w}{177.4\ \mathrm{kN}} \cdot \htmlClass{sym-H_w}{5.175\ \mathrm{m}} \\ &= 918.3\ \mathrm{kN} \cdot \mathrm{m} \end{aligned}\]
S.32 \[\begin{aligned} \htmlClass{sym-M_r}{M_{r}} &= \htmlClass{sym-P_r}{P_{r}} \cdot \htmlClass{sym-h_roof}{h_{\mathrm{roof}}} \\ &= \htmlClass{sym-P_r}{3.975\ \mathrm{kN}} \cdot \htmlClass{sym-h_roof}{10.35\ \mathrm{m}} \\ &= 41.14\ \mathrm{kN} \cdot \mathrm{m} \end{aligned}\]
S.33 \[\begin{aligned} \htmlClass{sym-M_i}{M_{i}} &= \htmlClass{sym-P_i}{P_{i}} \cdot \htmlClass{sym-h_i}{h_{i}} \\ &= \htmlClass{sym-P_i}{705.6\ \mathrm{kN}} \cdot \htmlClass{sym-h_i}{3.431\ \mathrm{m}} \\ &= 2.421\ \mathrm{MN} \cdot \mathrm{m} \end{aligned}\]
S.34 \[\begin{aligned} \htmlClass{sym-M_c}{M_{c}} &= \htmlClass{sym-P_c}{P_{c}} \cdot \htmlClass{sym-h_c}{h_{c}} \\ &= \htmlClass{sym-P_c}{118.5\ \mathrm{kN}} \cdot \htmlClass{sym-h_c}{5.357\ \mathrm{m}} \\ &= 635.1\ \mathrm{kN} \cdot \mathrm{m} \end{aligned}\]
S.35 \[\begin{aligned} \htmlClass{sym-M_eg}{M_{\mathrm{eg}}} &= \htmlClass{sym-P_eg}{P_{\mathrm{eg}}} \cdot \htmlClass{sym-h_eg}{h_{\mathrm{eg}}} \\ &= \htmlClass{sym-P_eg}{0\ \mathrm{kN}} \cdot \htmlClass{sym-h_eg}{0\ \mathrm{m}} \\ &= 0\ \mathrm{N} \cdot \mathrm{m} \end{aligned}\]
S.36 \[\begin{aligned} \htmlClass{sym-M_s}{M_{s}} &= \sqrt{\left(\htmlClass{sym-M_i}{M_{i}} + \htmlClass{sym-M_w}{M_{w}} + \htmlClass{sym-M_r}{M_{r}}\right)^{2} + \htmlClass{sym-M_c}{M_{c}}^{2} + \htmlClass{sym-M_eg}{M_{\mathrm{eg}}}^{2}} \\ &= \sqrt{\left(\htmlClass{sym-M_i}{2.421\ \mathrm{MN} \cdot \mathrm{m}} + \htmlClass{sym-M_w}{918.3\ \mathrm{kN} \cdot \mathrm{m}} + \htmlClass{sym-M_r}{41.14\ \mathrm{kN} \cdot \mathrm{m}}\right)^{2} + \left(\htmlClass{sym-M_c}{635.1\ \mathrm{kN} \cdot \mathrm{m}}\right)^{2} + \left(\htmlClass{sym-M_eg}{0\ \mathrm{N} \cdot \mathrm{m}}\right)^{2}} \\ &= 3.44\ \mathrm{MN} \cdot \mathrm{m} \end{aligned}\]
S.37 \[\begin{aligned} \htmlClass{sym-M_i_prime}{{M'}_{i}} &= \htmlClass{sym-P_i}{P_{i}} \cdot \htmlClass{sym-h_i_prime}{{h'}_{i}} \\ &= \htmlClass{sym-P_i}{705.6\ \mathrm{kN}} \cdot \htmlClass{sym-h_i_prime}{7.184\ \mathrm{m}} \\ &= 5.069\ \mathrm{MN} \cdot \mathrm{m} \end{aligned}\]
S.38 \[\begin{aligned} \htmlClass{sym-M_c_prime}{{M'}_{c}} &= \htmlClass{sym-P_c}{P_{c}} \cdot \htmlClass{sym-h_c_prime}{{h'}_{c}} \\ &= \htmlClass{sym-P_c}{118.5\ \mathrm{kN}} \cdot \htmlClass{sym-h_c_prime}{7.763\ \mathrm{m}} \\ &= 920.2\ \mathrm{kN} \cdot \mathrm{m} \end{aligned}\]
S.39 \[\begin{aligned} \htmlClass{sym-M_s_prime}{{M'}_{s}} &= \sqrt{\left(\htmlClass{sym-M_i_prime}{{M'}_{i}} + \htmlClass{sym-M_w}{M_{w}} + \htmlClass{sym-M_r}{M_{r}}\right)^{2} + \htmlClass{sym-M_c_prime}{{M'}_{c}}^{2}} \\ &= \sqrt{\left(\htmlClass{sym-M_i_prime}{5.069\ \mathrm{MN} \cdot \mathrm{m}} + \htmlClass{sym-M_w}{918.3\ \mathrm{kN} \cdot \mathrm{m}} + \htmlClass{sym-M_r}{41.14\ \mathrm{kN} \cdot \mathrm{m}}\right)^{2} + \left(\htmlClass{sym-M_c_prime}{920.2\ \mathrm{kN} \cdot \mathrm{m}}\right)^{2}} \\ &= 6.099\ \mathrm{MN} \cdot \mathrm{m} \end{aligned}\]
S.40 \[\begin{aligned} \htmlClass{sym-q_hy_base}{q_{\mathrm{hy},\mathrm{base}}} &= \htmlClass{sym-gamma_fluid}{\gamma_{\mathrm{fluid}}} \cdot \htmlClass{sym-h_fluid}{h_{\mathrm{fluid}}} \\ &= \htmlClass{sym-gamma_fluid}{9.81\ \mathrm{kN/m³}} \cdot \htmlClass{sym-h_fluid}{9.15\ \mathrm{m}} \\ &= 89.76\ \mathrm{kPa} \end{aligned}\]
S.41 \[\begin{aligned} \htmlClass{sym-p_wy}{p_{\mathrm{wy}}} &= \frac{\htmlClass{sym-S_ds}{S_{\mathrm{ds}}} \cdot \htmlClass{sym-I}{I} \cdot \htmlClass{sym-epsilon}{\epsilon} \cdot \htmlClass{sym-gamma_conc}{\gamma_{\mathrm{conc}}} \cdot \htmlClass{sym-t_wall}{t_{\mathrm{wall}}}}{\htmlClass{sym-R_wi}{R_{\mathrm{wi}}}} \\ &= \frac{\htmlClass{sym-S_ds}{1.06} \cdot \htmlClass{sym-I}{1.5} \cdot \htmlClass{sym-epsilon}{0.7041} \cdot \htmlClass{sym-gamma_conc}{23.56\ \mathrm{kN/m³}} \cdot \htmlClass{sym-t_wall}{650\ \mathrm{mm}}}{\htmlClass{sym-R_wi}{2}} \\ &= 8.572\ \mathrm{kPa} \end{aligned}\]
S.42 \[\begin{aligned} \htmlClass{sym-p_iy_base}{p_{\mathrm{iy},\mathrm{base}}} &= \frac{\left(4 \cdot \htmlClass{sym-h_fluid}{h_{\mathrm{fluid}}} - 6 \cdot \htmlClass{sym-h_i}{h_{i}}\right) \cdot \frac{\htmlClass{sym-P_i}{P_{i}}}{2}}{\htmlClass{sym-h_fluid}{h_{\mathrm{fluid}}}^{2} \cdot \htmlClass{sym-B}{B}} \\ &= \frac{\left(4 \cdot \htmlClass{sym-h_fluid}{9.15\ \mathrm{m}} - 6 \cdot \htmlClass{sym-h_i}{3.431\ \mathrm{m}}\right) \cdot \frac{\htmlClass{sym-P_i}{705.6\ \mathrm{kN}}}{2}}{\left(\htmlClass{sym-h_fluid}{9.15\ \mathrm{m}}\right)^{2} \cdot \htmlClass{sym-B}{1\ \mathrm{m}}} \\ &= 67.48\ \mathrm{kPa} \end{aligned}\]
S.43 \[\begin{aligned} \htmlClass{sym-p_iy_top}{p_{\mathrm{iy},\mathrm{top}}} &= \frac{\left(6 \cdot \htmlClass{sym-h_i}{h_{i}} - 2 \cdot \htmlClass{sym-h_fluid}{h_{\mathrm{fluid}}}\right) \cdot \frac{\htmlClass{sym-P_i}{P_{i}}}{2}}{\htmlClass{sym-h_fluid}{h_{\mathrm{fluid}}}^{2} \cdot \htmlClass{sym-B}{B}} \\ &= \frac{\left(6 \cdot \htmlClass{sym-h_i}{3.431\ \mathrm{m}} - 2 \cdot \htmlClass{sym-h_fluid}{9.15\ \mathrm{m}}\right) \cdot \frac{\htmlClass{sym-P_i}{705.6\ \mathrm{kN}}}{2}}{\left(\htmlClass{sym-h_fluid}{9.15\ \mathrm{m}}\right)^{2} \cdot \htmlClass{sym-B}{1\ \mathrm{m}}} \\ &= 9.64\ \mathrm{kPa} \end{aligned}\]
S.44 \[\begin{aligned} \htmlClass{sym-p_cy_base}{p_{\mathrm{cy},\mathrm{base}}} &= \frac{\left(4 \cdot \htmlClass{sym-h_fluid}{h_{\mathrm{fluid}}} - 6 \cdot \htmlClass{sym-h_c}{h_{c}}\right) \cdot \frac{\htmlClass{sym-P_c}{P_{c}}}{2}}{\htmlClass{sym-h_fluid}{h_{\mathrm{fluid}}}^{2} \cdot \htmlClass{sym-B}{B}} \\ &= \frac{\left(4 \cdot \htmlClass{sym-h_fluid}{9.15\ \mathrm{m}} - 6 \cdot \htmlClass{sym-h_c}{5.357\ \mathrm{m}}\right) \cdot \frac{\htmlClass{sym-P_c}{118.5\ \mathrm{kN}}}{2}}{\left(\htmlClass{sym-h_fluid}{9.15\ \mathrm{m}}\right)^{2} \cdot \htmlClass{sym-B}{1\ \mathrm{m}}} \\ &= 3.154\ \mathrm{kPa} \end{aligned}\]
S.45 \[\begin{aligned} \htmlClass{sym-p_cy_top}{p_{\mathrm{cy},\mathrm{top}}} &= \frac{\left(6 \cdot \htmlClass{sym-h_c}{h_{c}} - 2 \cdot \htmlClass{sym-h_fluid}{h_{\mathrm{fluid}}}\right) \cdot \frac{\htmlClass{sym-P_c}{P_{c}}}{2}}{\htmlClass{sym-h_fluid}{h_{\mathrm{fluid}}}^{2} \cdot \htmlClass{sym-B}{B}} \\ &= \frac{\left(6 \cdot \htmlClass{sym-h_c}{5.357\ \mathrm{m}} - 2 \cdot \htmlClass{sym-h_fluid}{9.15\ \mathrm{m}}\right) \cdot \frac{\htmlClass{sym-P_c}{118.5\ \mathrm{kN}}}{2}}{\left(\htmlClass{sym-h_fluid}{9.15\ \mathrm{m}}\right)^{2} \cdot \htmlClass{sym-B}{1\ \mathrm{m}}} \\ &= 9.801\ \mathrm{kPa} \end{aligned}\]

Questions

Why does R_wi reduce P_i but not P_c?

Impulsive mass moves with the walls at a short period, and ACI 350.3 lets that response be reduced by R_wi for the ductility and damping of the structure. Convective mass sloshes near the free surface at a long period, T_c, and is taken as an elastic response with R_wc = 1.0, so P_c is not reduced at all.

Why are P_i and P_c combined as a square root of the sum of squares in V?

The two respond at very different periods, so their peaks are not expected at the same instant. V adds the impulsive force, the walls and the roof directly, P_i + P_w + P_r, because they move together, then combines that with P_c and the earth pressure P_eg by square root of the sum of squares. M_s does the same with the moments.

Does the check on h_freeboard allow for the sloshing wave?

No. freeboard_adequate only checks that the fluid surface is below the top of the wall. ACI 350.3 gives the maximum sloshing height of a rectangular tank as d_max = (L/2) C_c I; compare that with h_freeboard yourself where the wave must not reach the roof or the wall top.

Why is B a unit width of 1 m?

The sheet works a one-metre strip of the tank across the direction of shaking, so W_fluid, W_i, W_c and every force and moment are per metre of tank width. Multiply by the tank's width for the whole tank, and note that W_walls counts only the two walls perpendicular to the shaking.