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E.6 Acoustic Solid Element

E.6.1 Convective Natural Frequencies in a Rigid Rectangular Tank

For a rigid rectangular tank containing a compressible fluid with length \(\small L_{x}\), width \(\small L_{y}\), and height \(\small H\), where the top surface is subject to a zero-pressure condition and all other surfaces are subject to a zero-flux condition, the following eigenvalues can be derived analytically.

\[ \small \begin{array}{r} \omega_{lmn} = c\sqrt{\alpha_{l}^{2} + \beta_{m}^{2} + \gamma_{n}^{2}}\tag{E.6.1} \end{array} \]

where

\(\small c\) is acoustic wave velocity, 1480 m/s/s if water

\(\small \alpha_{l} = \frac{l\pi}{L_{x}},\ \beta_{m} = \frac{m\pi}{L_{y}},\gamma_{n} = \frac{(2n - 1)\pi}{2H}\)

\(\small l,m = 0,1,2,\ldots,\ \ n = 1,2,\ldots\)

For a rectangular water tank with dimensions of 40 m (length), 30 m (width), and 20 m (height), a natural frequency analysis was performed under three-dimensional conditions using three different meshes, and the results were compared with the analytical solutions.

Figure E.6.1 Contour Plot of Mode Shapes

Table E.6.1 Natural Frequencies of 3D Rigid Rectangular Tank

l m n Analytic solution Numerical solution
alpha beta gamma wlnm frq 8x4 12x6 16x8 16x12-P6 16x12-P8 16x12-P8+T4
010000.07854116.238928218.500018.619118.552918.529718.524218.5259
1000.0785400164.386668726.163026.331426.237726.205426.175826.1755
2000.1570800193.731549730.833331.13130.965430.907630.900831.0321
02000.157080225.296757535.963136.247436.065335.949635.936936.3651
1100.078540.078540259.91814541.367342.277541.770441.593741.509942.0162
001000.07854302.618530448.163249.000348.573848.393848.697249.1273
2100.157080.078540343.019461653.168054.360353.202853.282753.4984
1200.078540.157080348.716784555.003857.395756.767656.305556.150456.2974
01100.078540.07854350.86572455.841556.993556.365156.143156.193956.1939
1110.078540.078540.07854357.579765858.502161.615759.821759.076459.591159.91
3000.23561900367.579765858.502161.615759.821759.076459.591159.91
2200.157080.157080381.808961660.734663.652261.499961.539962.0894
3100.2356190.104720.07854398.917670963.4997266.476564.8164.230764.627865.3594
1300.078540.2356190.10472399.917670963.4997266.476564.8164.230764.627865.3594
2120.157080.209440.07854404.523346264.381966.712865.413464.968065.140465.5128
2020.1570800.235619419.105415866.702769.933568.133567.505567.094969.9077

For a rectangular water tank with dimensions of 40 m (width) and 20 m (height), a natural frequency analysis was performed under two-dimensional conditions using three different meshes, and the results were compared with the analytical solutions. In the analytical solutions, the case of \(\small m = 0\) was always considered.

Table E.6.2 Natural Frequencies of 2D Rigid Rectangular Tank

l m n Analytic solution Numerical solution
alpha beta gamma wlnm frq 8x4 12x6 16x8 16x8-T
100000.07854116.238928218.500018.619118.552918.529718.5296
1010.0785400.07854164.386668726.163026.331426.237726.205426.2881
2010.1570800.07854259.91814541.367342.277541.770441.593741.8000
02000.2356190348.716784555.000058.736556.935256.305556.2984
3000.23561900.07854367.579765858.502161.61759.821759.276159.5851
2100.078540.2356190419.105415866.702769.93468.632567.653568.6724
4000.31415900.07854479.265378776.277583.06679.601778.142378.3488
3020.23561900.235619493.160060178.488983.69480.518579.628182.91

Input File

  • tank2d-8x4.inp : 2 dimensional rectangular tank, 8x4 elements, AC2D4

  • tank2d-12x6.inp : 2 dimensional rectangular tank, 12x6 elements, AC2D4

  • tank2d-16x8.inp : 2 dimensional rectangular tank, 16x8 elements, AC2D4

  • tank2d-16x8-T3.inp : 2 dimensional rectangular tank, 16x8*2 elements, AC2D3

  • tank3d-8x6x4.inp : 3 dimensional rectangular tank, 8x6x4 elements, AC3D8

  • tank3d-12x9x6.inp : 3 dimensional rectangular tank, 12x9x6 elements, AC3D8

  • tank3d-16x12x8.inp : 3 dimensional rectangular tank, 16*12*8 elements, AC3D8

  • tank3d-16x12x8-T4.inp : 3 dimensional rectangular tank, 16*12*8*6 elements, AC3D4

  • tank3d-16x12x8-P6.inp : 3 dimensional rectangular tank, 16*12*8*2 elements, AC3D6

E.6.2 Sloshing Natural Frequencies in a Rigid Rectangular Tank

For an incompressible fluid, the natural frequencies of free-surface sloshing in a rectangular tank can be derived analytically (Lamb, 1945).

\[ \small \begin{array}{r} \omega_{mn} = \sqrt{gk_{mn}\tanh\left( k_{mn}H \right)}\tag{E.6.2} \end{array} \]

where

\[ \small \begin{array}{r} \ k_{mn} = \sqrt{\alpha_{m}^{2} + \beta_{n}^{2}},\ \ \alpha_{m} = \frac{m\pi}{L_{x}},\ \ \beta_{n} = \frac{n\pi}{L_{y}},\ where\ \ l,m = 0,1,2,\ldots,\ \ n = 1,2,\ldots\tag{E.6.3} \end{array} \]

Housner (1957) proposed the following approximate formula for the fundamental frequency.

\[ \small \begin{array}{r} \omega^{2} = \frac{g}{L/2}\sqrt{\frac{5}{2}}\tanh\left( \sqrt{\frac{5}{2}}\frac{H}{L/2}\ \right)\tag{E.6.4} \end{array} \]

Here, \(\small L\) is the length in the direction of excitation.

Table E.6.3 Natural Frequencies of Sloshing Modes in 3D Rigid Rectangular Tank

m n kmn f Numerical solution
10x30x6 20x60x11 20x60x11-P6 20x60x11 20x60x11-T4
000.0000.0000000
010.0530.0840.0844160.0843680.0843680.084372
020.1070.1490.1490680.1487960.1487830.148874
100.1600.1940.1950560.194390.1943290.194702
030.1600.1940.1950560.194390.1943430.195071
110.1690.2000.2012260.2005510.2005360.201349
120.1930.2160.2169470.2161810.2162380.217327
040.2140.2290.2302640.2290040.2288740.229771
130.2270.2360.2373130.2362660.2363720.237929
050.2670.2570.2591960.2576120.2575360.258952
140.2670.2570.2599090.2577870.2577340.260181
150.3120.2780.2813210.2789010.2789680.281839
060.3210.2820.2865570.2832470.2828610.285658
200.3210.2820.2865570.2832470.2828620.287921
210.3250.2840.288540.2852160.2848790.290092
220.3380.2900.2942890.2908930.2906920.296245

Table E.6.4 Natural Frequencies of Sloshing Modes in 2D Rigid Rectangular Tank

m km f Numerical solution
30x6 60x11 60x11-T
00.0000.000000
10.0530.0840.0844160.0843680.084372
20.1070.1490.1490680.1487960.148875
30.1600.1940.1950560.194390.194722
40.2140.2290.2302640.2290040.229799
50.2670.2570.2599090.2577870.259258
60.3210.2820.2865570.2832470.285611
70.3740.3050.3114380.3065720.310062
80.4270.3260.3352030.3238750.333244
90.4810.3460.3582470.3490170.355533
100.5340.3640.3808450.3687380.377183
110.5880.3820.4032040.3877120.398377

Input File

  • sloshing2d-30x6.inp : 2 dimensional rectangluar tank, 30*6 elements, AC2D4

  • sloshing2d-60x11.inp : 2 dimensional rectangluar tank, 60*11 elements, AC2D4

  • sloshing2d-60x11-T3.inp : 2 dimensional rectangluar tank, 60*11*2 elements, AC2D3

  • sloshing3d-10x30x6.inp : 3 dimensional rectangluar tank, 10*30*6 elements, AC3D8

  • sloshing3d-20x60x11.inp : 3 dimensional rectangluar tank, 20*60*11 elements, AC3D8

  • sloshing3d-20x60x11-T4.inp : 3 dimensional rectangluar tank, 20*60*11*6 elements, AC3D4

  • sloshing3d-20x60x11-P6.inp : 3 dimensional rectangluar tank, 20*60*11*6 elements, AC3D6

E.6.3 Natual Frequencies in a Rigid Cylinderical Tank

For a cylindrical tank, various natural frequencies were calculated. The exact solution for sloshing is given as follows.

(1) Veletos (1984) proposed the following equation.

\[ \small \begin{array}{r} \omega_{j}^{2} = \frac{\lambda_{j}g}{R}\tanh\left( \lambda_{j}\frac{H}{R}\ \right)\tag{E.6.5} \end{array} \]

여기에서 \(\small \lambda_{j}\)\(\small \frac{dJ_{1}(x)}{dx} = 0\)의 해이며, 저차 3개 값은 \(\small \lambda_{1} = 1.8411837813406593\), \(\small \lambda_{2} = 5.331442773525033\), \(\small \lambda_{3} = 8.536316366346286\) 이다.

(2) Housner (1957) proposed the following approximate formula for the fundamental frequency of sloshing.

\[ \small \begin{array}{r} \omega^{2} = \frac{g}{R}\sqrt{\frac{27}{8}}\ \tanh\left( \sqrt{\frac{27}{8}}\frac{H}{R}\ \right)\tag{E.6.6} \end{array} \]

All sloshing frequencies are based on the assumption of incompressible water. When compressibility is considered, however, the exact solution for the impulsive component is the same as that for a rectangular tank with \(L_{x} = L_{y} = 2R\).

Solutions were compared for both a wide cylinder and a tall cylinder. The wide cylinder has \(R = 18.3\ \text{m}\) and \(H = 12.2\ \text{m}\), while the tall cylinder has \(R = 10\ \text{m}\) and \(H = 30\ \text{m}\). Two mesh types were prepared for each case, and the fundamental frequencies were compared.

Table E.6.5 Sloshing Freqencies of wideCylinder Model

Numerical Solution Analytic Solution
Model Natural Frequency
wideCylinderIncomp-15x10 0.145258 Hz

0.145075 Hz(Veletsos),

0.144846 Hz((Housner)

wideCylinder-15x10 0.145256 Hz
wideCylinderIncomp-30x15 0.14516 Hz
wideCylinder-30x15 0.145158 Hz

Table E.6.6 Impulsive Frequencies of wideCylinder Model

Numerical Solution Analytic Solution
Model Natural Frequency
wideCylinder-15x10 30.3591 Hz 30.3279 Hz
wideCylinder-30x15 30.3417 Hz

Figure E.6.2 Sloshing Mode of wideCylinder-20.x10

Figure E.6.3 Impulsive Mode of wideCylinder-20.x10

Table E.6.7 Solshing Freuencies of tallCylinder Model

Numerical Solution Analytic Solution
Model Natural Frequency
tallCylinderIncomp-10x10 0.21567 Hz

0.21389 Hz(Veletsos),

0.213656 Hz((Housner)

tallCylinder-10x10 0.215668 Hz
tallCylinderIncomp-15x15 0.21567 Hz
tallCylinder-15x15 0.215668 Hz

Table E.6.8 Impulsive Frequencies of tallCylinder Model

Numerical Solution Analytic Solution
Model Natural Frequency
tallCylinder-10x10 12.346 Hz 12.3333 Hz
tallCylinder-15x15 12.346 Hz

Figure E.6.4 Sloshing Mode of tallCylinder-10.x10

Figure E.6.5 Impulsive Mode of tallCylinder-10.x10

Input File

  • wideCylinder-20x10.inp : Wide Cylinder with 20*10 elements

  • wideCylinderIncomp-20x10.inp : Wide Cylinder with 20*10 elements, Incompressible Water

  • wideCylinder-30x15.inp : Wide Cylinder with 30*15 elements

  • wideCylinderIncomp-30x15.inp : Wide Cylinder with 30*15 elements, Incompressible Water

  • tallCylinder-10x10.inp : Tall Cylinder with 10*10 elements

  • tallCylinderIncomp-10x10.inp : Tall Cylinder with 10*10 elements, Incompressible Water

  • tallCylinder-15x15.inp : Tall Cylinder with 15*15 elements

  • tallCylinderIncomp-15x15.inp : Tall Cylinder with 15*15 elements, Incompressible Water

References

  1. Lamb, H. (1945) Hydrodynamics, 6th Edition, Dover Publications.

  2. Veletos, A.S.(1984), Seismic reesponse and design of liquid storage tanks, Guidelines for the seismic design of oil and gas pipeline systems, ASCE

  3. Housner, G. W. (1957). Dynamic pressures on accelerated fluid containers. Bulletin of the seismological society of America, 47(1), 15-35.