题 1

一无限流体被单位质量力 μr3/2\mu r^{-3/2} 的力作用,方向指向原点。若开始时流体静止且其中有一个空腔 r=cr=c,证明:在过 (25μ)1/2c5/4(\frac{2}{5 \mu})^{1/2} c^{5/4} 时间之后,空腔被流体填满。

这里假设流体不可压缩。取球坐标系 (r,θ,ϕ)(r, \theta, \phi) 进行计算,并以空腔中心为原点。

思路1:功能关系

假设当 t=t0t=t_0 时,空腔边界的球壳形薄液面位于 r=r0r=r_0 处。该薄液面厚度为 dr0\mathrm{d}r_0, 液面速度 vr(r0,t0)=0v_r (r_0, t_0) = 0

t0t_0 时刻,位于 r=r0r=r_0 处且厚度为 dr0\mathrm{d}r_0 的液面向内推动了 dr\mathrm{d} r, 由于该液面的质量积为 dm=ρ(4πr02)dr0\mathrm{d}m = \rho (4 \pi r_0^2) \mathrm{d}r_0,则这一过程中体积力(Fbr=μr3/2F_{br} = -\mu r^{-3/2})所作的功为

dW=dmr0+Fbrdr=dm(2μr01/2)=8μρπr03/2dr0.\mathrm{d} W = \mathrm{d}m \cdot \int_{r_0}^{+\infty} F_{br} \mathrm{d}r = \mathrm{d}m \cdot (-2 \mu r_0^{-1/2}) = -8 \mu \rho \pi r_0^{3/2} \mathrm{d}r_0 .

t1=t0+δtt_1 = t_0 + \delta_t 时,该液面前进到 r=r1r=r_1 位置(r1r0r_1 \le r_0),此时液面速度为 vr(r1,t1)=dr1dtv_r(r_1, t_1) = \dfrac{\mathrm{d} r_1}{\mathrm{d} t}

所以薄液面从 r0r_0 运动到 r1r_1 过程中, FbrF_{br} 做的总功为:

W=r0r1dW=165μρπ(r05/2r15/2)W = \int_{r_0}^{r_1} \mathrm{d} W = \frac{16}{5} \mu \rho \pi (r_0^{5/2} - r_1^{5/2})

记速度 v=[vr,0,0]T\bold{v} = [v_r, 0, 0]^T。代入球坐标系下的连续性方程,化简得:

(r2vr)r=0\frac{\partial (r^2 v_r)}{\partial r} = 0

rr 积分,可得 r2vr=f(t)r^2 v_r = f(t) ,其中 f(t)f(t) 为待定函数。根据这一方程,可得在 t1t_1 时刻满足 r02vr(r0,t1)=r12vr(r1,t1)r_0^2 v_r(r_0, t_1) = r_1^2 v_r(r_1, t_1)

t1t_1 时刻, r=r0r=r_0 层液体的动能表示为

dE=12dmvr2(r0,t1)=2ρπr14r02vr2(r1,t1)dr0\mathrm{d} E = \frac{1}{2} \cdot \mathrm{d}m \cdot v_r^2(r_0, t_1) = 2 \rho \pi \cdot \frac{r_1^4}{r_0^2} \cdot v_r^2(r_1, t_1) \mathrm{d}r_0

这一时刻下整个系统的动能为:

E=r1+dE=2ρπr13vr2(r1,t1)E = \int_{r_1}^{+\infty} \mathrm{d} E = 2 \rho \pi r_1^3 \cdot v_r^2(r_1, t_1)

据此,我们令 t0t_0 时刻即为初始时刻(t0=0t_0=0),满足 r0=cr_0 = cvr(t=0)=0v_r(t=0)=0。所以 t0t_0 时刻的动能为 0。对 t0t_0t1t_1 时刻的过程, FbrF_{br} 所做的功 WW 全部转化为流场动能 EE,即:W=EW=E

165μρπ(c5/2r15/2)=2ρπr13vr2(r1,t1)0\frac{16}{5} \mu \rho \pi (c^{5/2} - r_1^{5/2}) = 2 \rho \pi r_1^3 \cdot v_r^2(r_1, t_1) - 0

也就有:

vr(r1,t1)=dr1dt=8μ5r13/2(c5/2r15/2)v_r(r_1, t_1) = \frac{\mathrm{d} r_1}{\mathrm{d} t} = \sqrt{\frac{8 \mu}{5}} \cdot \sqrt{r_1^{-3/2} (c^{5/2} - r_1^{5/2})}

分离变量后解得:

1625(c5/2r15/2)=(8μ5t+c1)2\frac{16}{25} (c^{5/2} - r_1^{5/2}) = \left( \sqrt{\frac{8 \mu}{5}} t + c_1 \right)^2

其中 c1c_1 为待定常数。当 t=0t=0 时, r1=cr_1 = c,所以 c1=0c_1 = 0

假设当 t=Tmt=T_{m}r1=0r_1=0, 则可解得: Tm=(25μ)1/2c5/4T_m = (\frac{2}{5 \mu})^{1/2} c^{5/4}

思路2:联立动量方程和连续性方程

记速度 v=[vr,0,0]T\bold{v} = [v_r, 0, 0]^T。代入连续性方程,化简得:

(r2vr)r=0\frac{\partial (r^2 v_r)}{\partial r} = 0

rr 积分,可得 r2vr=f(t)r^2 v_r = f(t) ,其中 f(t)f(t) 为待定函数。

该场景下的运动方程为

ρDvDt=ρFb\rho \frac{\mathrm{D} \bold{v}}{\mathrm{D} t} = \rho \bold{F}_b

所以,动量方程写作:

vrt+vrvrr=Fbr\frac{\partial v_r}{\partial t} + v_r \frac{\partial v_r}{\partial r} = F_{br}

由题目可知 Fbr=μr3/2F_{br} = - \mu r^{-3/2}。将 r2vr=f(t)r^2 v_r = f(t) 代入到运动方程中,得:

f(t)r2+vrvrr=μr3/2\frac{f'(t)}{r^2} + v_r \frac{\partial v_r}{\partial r} = -\mu r^{-3/2}

R(t)R(t) 为真空球面的半径变化,则 vr(r=R(t))=R(t)v_r (r=R(t)) = R'(t)。对 rr 积分,得到:

R(t)f(t)r2+vrvrrdr=μR(t)r3/2dr[f(t)r+(vr)22]R(t)=2μrR(t)\begin{aligned} \int_{\infty}^{R(t)} \frac{f'(t)}{r^2} + v_r \frac{\partial v_r}{\partial r} \mathrm{d}r &= -\mu \int_{\infty}^{R(t)} r^{-3/2} \mathrm{d}r \\ \left.\left[ -\frac{f'(t)}{r} + \frac{(v_r)^2}{2} \right]\right|_{\infty}^{R(t)} &= \left. \frac{2 \mu}{\sqrt{r}} \right|_{\infty}^{R(t)} \end{aligned}

代入 vr(r=)=0v_r (r=\infty)=0,整理得到:

f(t)R(t)+(R(t))22=2μR(t)-\frac{f'(t)}{R(t)} + \frac{(R'(t))^2}{2} = \frac{2 \mu}{\sqrt{R(t)}}

在边界上有 f(t)=R2(t)vr(r=R(t))=R2Rf(t) = R^2(t) \cdot v_r (r=R(t)) = R^2 \cdot R' , 所以 f(t)=2RR2+R2Rf'(t) = 2 R R'^{2} + R^2 \cdot R{''} 。上式化简为:

32R2RR=2μR-\frac{3}{2} R'^{2} -R \cdot R{''} = \frac{2 \mu}{\sqrt{R}}

由于 d(R1/2(R)2)dR=R1/22(R)2+2R1/2R\frac{\mathrm{d} (R^{1/2} (R')^{2})}{\mathrm{d} R} =\frac{R^{-1/2}}{2} (R')^{2} + 2 R^{1/2} R{''},上式整理得:

d(R1/2(R)2)8μ+5(R1/2(R)2)=dR2R-\frac{\mathrm{d}(R^{1/2} (R')^{2})}{8\mu + 5 (R^{1/2} (R')^{2})} = \frac{\mathrm{d}R}{2R}

分离变量后并整理出 RR' ,可表示为:

R=R1/25(c1R5/28μ)R' = \sqrt{\frac{R^{-1/2}}{5} (c_1 R^{-5/2} - 8 \mu) }

R(t=0)=cR(t=0)=cR(t=0)=0R'(t=0) = 0 代入,解得: c1=8μc5/2c_1 = 8 \mu c^{5/2} 。即:

R=R1/258μ(c5/2R5/21)=8μ5R1/2(c5/2R5/21)R' = \sqrt{\frac{R^{-1/2}}{5} 8 \mu (c^{5/2} R^{-5/2} - 1)} \\= \sqrt{\frac{8 \mu}{5}} \cdot \sqrt{R^{-1/2} (c^{5/2} R^{-5/2} - 1)}

综上,真空球面的总运动时长表示为:

T=0c1RdR=58μ0c[R1/2((cR)5/21)]1/2dRT = \int_{0}^{c} \frac{1}{R'} \mathrm{d}R = \sqrt{\frac{5}{8 \mu}} \int_{0}^{c} \left[ R^{-1/2} \left( \left(\frac{c}{R}\right)^{5/2} - 1 \right) \right]^{-1/2} \mathrm{d}R

因为:

0c[R1/2((cR)5/21)]1/2dR=0cR1/4[((cR)5/21)]1/2dR=450c[((cR)5/21)]1/2d(R5/4)=t=R5/4450c5/4[(c5/2t21)]1/2dt=450c5/4t[(c5/2t2)]1/2dt=45(12)0c5/4[(c5/2t2)]1/2d(c5/2t2)=45(12)2(c5/2t2)1/20c5/4=45c5/4\begin{aligned} & \int_{0}^{c} \left[ R^{-1/2} \left( \left(\frac{c}{R}\right)^{5/2} - 1 \right) \right]^{-1/2} \mathrm{d}R \\ =& \int_{0}^{c} R^{1/4} \left[ \left( \left(\frac{c}{R}\right)^{5/2} - 1 \right) \right]^{-1/2} \mathrm{d}R \\ =& \frac{4}{5} \int_{0}^{c} \left[ \left( \left(\frac{c}{R}\right)^{5/2} - 1 \right) \right]^{-1/2} \mathrm{d}(R^{5/4}) \\ \xlongequal{t=R^{5/4}} & \frac{4}{5} \int_{0}^{c^{5/4}} \left[ \left( c^{5/2} t^{-2} - 1 \right) \right]^{-1/2} \mathrm{d}t \quad= \frac{4}{5} \int_{0}^{c^{5/4}} t \left[ \left( c^{5/2} - t^2 \right) \right]^{-1/2} \mathrm{d}t \\ =& \frac{4}{5} \cdot \left(-\frac{1}{2}\right) \int_{0}^{c^{5/4}} \left[ \left( c^{5/2} - t^2 \right) \right]^{-1/2} \mathrm{d}(c^{5/2} - t^2) \\ =& \frac{4}{5} \cdot \left(-\frac{1}{2}\right) \left.2 (c^{5/2} - t^2)^{1/2}\right|_{0}^{c^{5/4}} = \frac{4}{5} c^{5/4} \end{aligned}

所以 T=58μ45c5/4=25μc5/4T = \sqrt{\frac{5}{8 \mu}} \cdot \frac{4}{5} c^{5/4} = \sqrt{\frac{2}{5 \mu}} c^{5/4} .

证毕。

题 2

体积为 43πa3\frac{4}{3} \pi a^3 的液体充满于两个同心球面之间,外球面有压强 π\pi 作用,无质量力,内球面压强为 0 。开始时液体静止,内球面半径为 2a2a 。证明:当内球面半径变为 aa 时,其速度为 (14π3ρ21/321/31)12\displaystyle \left(\frac{14 \pi}{3 \rho} \frac{2^{1/3}}{2^{1/3} - 1}\right)^{\frac{1}{2}}

这里假设流体不可压缩。取球坐标系 (r,θ,ϕ)(r, \theta, \phi) 进行计算,并以空腔中心为原点。

记初始状态下(即 t=0t=0 时刻),内球面半径为 R0=2aR_0=2 a,外球面半径为 R1R_1;当内球面半径变为 aa 时(即 t1t_1 时刻),此时的内、外球面半径为分别为 R01=aR_{01} = aR11R_{11}。由于流体体积 V=43πa3V = \frac{4}{3} \pi a^3,可得:

V=43π(R13R03)=43π(R113R013)\begin{aligned} V &= \frac{4}{3} \pi (R_1^3 - R_0^3) \\ &= \frac{4}{3} \pi (R_{11}^3 - R_{01}^3) \end{aligned}

解得: R1=91/3aR_1 = 9^{1/3} aR11=21/3aR_{11} = 2^{1/3} a

记速度 u=[vr,0,0]T\bold{u} = [v_r, 0, 0]^T。代入连续性方程,化简得:

(r2vr)r=0\frac{\partial (r^2 v_r)}{\partial r} = 0

rr 积分,可得 r2vr=f(t)r^2 v_r = f(t) ,其中 f(t)f(t) 为待定函数。

t[0,t1]t \in [0,t_1] 时间段,外界压强在外表面做的功为:

W=R1R11(π)S(r)dr=283π2a3W = \int_{R_{1}}^{R_{11}} (-\pi) S(r) \mathrm{d} r = \frac{28}{3} \pi^2 a^3

其中 S(r)=4πr2S(r) = 4 \pi r^2 为球的表面积公式。

t1t_1 时刻, r2vr=f(t1)r^2 v_r = f(t_1) 为定值。若记此时刻的内球面速度为 u0=[v0,0,0]T\bold{u}_0 = [v_0, 0, 0]^Trr 处的流体速度为 ur=[vr,0,0]T\bold{u}_r = [v_r, 0, 0]^Tr[R01,R11]r \in [R_{01}, R_{11}]),则 R012v0=r2vrR_{01}^2 v_0 = r^2 v_r 。 所以 vr=(R01r)2v0v_r = \left( \frac{R_{01}}{r} \right)^2 v_0

t1t_1 时刻的流场总动能表示为:

Et1=R01R1112vr2(ρS(r)dr)=2πρv02a321/3121/3E_{t_1} = \int_{R_{01}}^{R_{11}} \frac{1}{2} v_r^2 \cdot (\rho S(r) \mathrm{d}r) = 2 \pi \rho v_0^2 a^3 \frac{2^{1/3} - 1}{2^{1/3}}

由于初始时刻的动能 E0=0E_0 = 0,根据功能关系可知:

W=Et1E0W = E_{t_1} - E_0

解得 t1t_1 时刻的内球面速度为: v0=(14π3ρ21/321/31)12\displaystyle v_0= - \left(\frac{14 \pi}{3 \rho} \frac{2^{1/3}}{2^{1/3} - 1}\right)^{\frac{1}{2}} ,方向指向原点。

本文同步发表于知乎CSDN

我在阅读其他文献时,看到有文献提到 Kupershtokh 的一篇关于 LBM 外力项的文章[1],他提出的格式在其他文章中又被称为 Exact difference method(EDM)

本想搜索这篇文章的PDF进行阅读,但最后只找到一个网站介绍了部分信息。这份粗略笔记的内容,都是基于其他文献[2][3][4]中对该方法的介绍而整理的。

介绍

Boltzmann-BGK方程的近似

密度分布函数 ff 的 Boltzmann-BGK方程写作:

ft+ξf+aξf=1τf[ff(eq)](1)\frac{\partial f}{\partial t} + \bold{\xi} \cdot \nabla f + \boldsymbol{a} \cdot \nabla_{\bold{\xi}} f = -\frac{1}{\tau_f} \left[ f - f^{(eq)}\right] \tag{1}

其中:

f(eq)=ρ(2πRgT)D/2exp((ξu)22RgT)(2)f^{(eq)} = \frac{\rho}{(2 \pi R_g T)^{D/2}} \exp{\left(- \frac{(\bold{\xi} - \bold{u})^2}{2 R_g T}\right)} \tag{2}

符号含义分别为

  • ξ\bold{\xi} : 粒子速度;
  • ρ\rho : 流体密度;
  • u\bold{u} : 流场宏观速度;
  • RgR_g : 气体常数;
  • TT : 温度;
  • a=du/dt\boldsymbol{a}=\mathrm{d}\bold{u}/\mathrm{d}t : 流场加速度。

Knudsen数较小时,Boltzmann方程的体力项可以基于f(eq)f^{(eq)}进行近似,即

ξfξf(eq)\nabla_{\bold{\xi}} f \approx \nabla_{\bold{\xi}} f^{(eq)}

根据式(2), f(eq)f^{(eq)} 是分子随机速度 C=ξu\bold{C} = \bold{\xi} - \bold{u} 的指数函数,则:

f(eq)u=f(eq)ξ=ξf(eq)\frac{\partial f^{(eq)}}{\partial \bold{u}} = -\frac{\partial f^{(eq)}}{\partial \bold{\xi}} = -\nabla_{\bold{\xi}} f^{(eq)}

假设密度 ρ\rho 为常数,则 dρdt=0\frac{\mathrm{d} \rho}{\mathrm{d} t}=0,那么 f(eq)f^{(eq)} 的全导数为:

df(eq)dt=f(eq)ududt+f(eq)ρdρdtf(eq)ududt=aξf(eq)\begin{aligned} \frac{\mathrm{d} f^{(eq)}}{\mathrm{d} t} &= \frac{\partial f^{(eq)}}{\partial \bold{u}} \cdot \frac{\mathrm{d} \bold{u}}{\mathrm{d} t} + \frac{\partial f^{(eq)}}{\partial \rho} \cdot \frac{\mathrm{d} \rho}{\mathrm{d} t} \\ &\approx \frac{\partial f^{(eq)}}{\partial \bold{u}} \cdot \frac{\mathrm{d} \bold{u}}{\mathrm{d} t} = -\boldsymbol{a} \cdot \nabla_{\bold{\xi}} f^{(eq)} \end{aligned}

也就是说,Kupershtokh 等[1:1][2:1]近似的 Boltzmann-BGK方程写作:

ft+ξf=1τf[ff(eq)]+df(eq)dt(3)\frac{\partial f}{\partial t} + \bold{\xi} \cdot \nabla f = -\frac{1}{\tau_f} \left[ f - f^{(eq)}\right] + \frac{\mathrm{d} f^{(eq)}}{\mathrm{d} t} \tag{3}

近似方程的离散化

将式(3)在[t,t+δt][t,t+\delta_t]内沿着eα\bold{e}_\alpha方向积分,可得

fα(x+eαδt,t+δt)fα(x,t)=1τ[fα(x,t)fα(eq)(ρ,u)]+[fα(eq)(u(t+δt))fα(eq)(u(t))](4)\begin{aligned} f_\alpha (\bold{x} + \bold{e}_\alpha \delta_t, t+\delta_t) - f_\alpha (\bold{x}, t) =& -\frac{1}{\tau} \left[ f_\alpha (\bold{x}, t) - f_\alpha^{(eq)} (\rho, \bold{u^*}) \right] \\ & + \left[ f_\alpha^{(eq)} (\bold{u^*}(t+\delta_t)) - f_\alpha^{(eq)} (\bold{u^*}(t)) \right] \end{aligned} \tag{4}

其中:

  • δt\delta_t 为时间步长;
  • τ=τf/δt\tau = \tau_f / \delta_t 为无量纲松弛时间;
  • x\bold{x} 为网格点位置,ρ,u\rho, \bold{u^*} 分别为该点在 tt 时刻的密度和速度(与宏观速度 u\bold{u} 有区别);
  • fα,fα(eq)f_\alpha, f_\alpha^{(eq)} 分别为 eα\bold{e}_\alpha 方向的分布函数平衡态

fα(eq)=wαρ[1+eαucs2+(eαu)22cs4u22cs2]=wαρ[1+eαucs2+12cs4(uu):(eαeαcs2[I])](4-1)\begin{aligned} f_\alpha^{(eq)} &= w_\alpha \rho \cdot \left[ 1 + \frac{\bold{e}_\alpha \cdot \bold{u}}{c_s^2} + \frac{(\bold{e}_\alpha \cdot \bold{u})^2}{2 c_s^4} - \frac{|\bold{u}|^2}{2 c_s^2} \right] \\ &= w_\alpha \rho \cdot \left[ 1 + \frac{\bold{e}_\alpha \cdot \bold{u}}{c_s^2} + \frac{1}{2 c_s^4}(\bold{u}\bold{u}):(\bold{e}_\alpha \bold{e}_\alpha - c_s^2 [\bold{I}]) \right] \\ \end{aligned} \tag{4-1}

这里 wαw_\alphaeα\bold{e}_\alpha 的权重系数, [I][\bold{I}] 为单位矩阵;
两个同样为m*n大小的矩阵 [A][\bold{A}][B][\bold{B}] ,则 [A]:[B]=i=1mj=1nAijBij\displaystyle [\bold{A}] : [\bold{B}] = \sum^{m}_{i=1}\sum^{n}_{j=1} A_{ij} B_{ij}

  • FαF_\alpha 为外力项,其表达式基于外力 F=ρdudt=ρa\bold{F} = \rho \dfrac{\mathrm{d} \bold{u^*}}{\mathrm{d} t} = \rho \bold{a} 进行构建。

Fα=fα(eq)(u(t+δt))fα(eq)(u(t))F_\alpha = f_\alpha^{(eq)} (\bold{u^*}(t+\delta_t)) - f_\alpha^{(eq)} (\bold{u^*}(t))

并且

u(t)=(αfαeα)/(αfα)u(t+δt)=u(t)+tt+δtdudtdt=u(t)+tt+δtFρdtu(t)+Fρδt(5)\begin{aligned} \bold{u^*}(t) &= \left(\sum_{\alpha} f_\alpha \bold{e}_\alpha \right) / \left(\sum_{\alpha} f_\alpha \right) \\ \bold{u^*}(t+\delta_t) &= \bold{u^*}(t) + \int_{t}^{t+\delta_t} \frac{\mathrm{d} \bold{u^*}}{\mathrm{d} t} \mathrm{d} t \\ &= \bold{u^*}(t) + \int_{t}^{t+\delta_t} \frac{\bold{F}}{\rho} \mathrm{d} t \approx \bold{u^*}(t) + \frac{\bold{F}}{\rho} \delta_t \end{aligned} \tag{5}

这意味着加速度 a=F/ρ\bold{a}=\bold{F}/\rho[t,t+δt][t,t+\delta_t] 时间段内被视为常数。

Kupershtokh等在这篇文章[2:2]说明,在使用该源项时,流体宏观量的计算应表示为:

ρ=αfα,ρu=ieαfα+δtF2(6)\rho = \sum_{\alpha} f_\alpha ,\quad \rho \bold{u} = \sum_{i} \bold{e}_\alpha f_\alpha + \frac{\delta_t \bold{F}}{2} \tag{6}

Li 等[4:1]通过 Chapman-Enskog 展开证明:该格式向宏观方程引入的误差项为:

ErrorEDM=δt2(FF4ρ)(7)\mathbf{Error}_{\mathrm{EDM}} = -\delta_t^2 \nabla\cdot\left( \frac{\bold{FF}}{4 \rho} \right) \tag{7}

EDM 源项的展开式

为便于分析,这里采用如下书写形式的平衡态:

fα(eq)=wαρ[1+eαucs2+12cs4(uu):(eαeαcs2[I])]f_\alpha^{(eq)} = w_\alpha \rho \cdot \left[ 1 + \frac{\bold{e}_\alpha \cdot \bold{u}}{c_s^2} + \frac{1}{2 c_s^4}(\bold{u}\bold{u}):(\bold{e}_\alpha \bold{e}_\alpha - c_s^2 [\bold{I}]) \right]

将其带入 EDM 源项,记 Δu=Fρδt\Delta\bold{u} = \frac{\bold{F}}{\rho} \delta_t,整理得:

Fα=fα(eq)(u(t+δt))fα(eq)(u(t))=ρwα{eαΔucs2+12cs4[(u+Δu)(u+Δu)uu]:(eαeαcs2[I])}\begin{aligned} F_{\alpha} &= f_\alpha^{(eq)} (\bold{u^*}(t+\delta_t)) - f_\alpha^{(eq)} (\bold{u^*}(t)) \\&= \rho w_\alpha \left\{ \frac{\bold{e}_\alpha \cdot \Delta\bold{u}}{c_s^2} + \newline \frac{1}{2 c_s^4} \left[ (\bold{u}^* + \Delta\bold{u})(\bold{u}^* + \Delta\bold{u}) \right.\right. \\ &\quad \left. - \bold{u}^* \bold{u}^* \right] : \left.(\bold{e}_\alpha \bold{e}_\alpha - c_s^2 [\bold{I}]) \right\} \end{aligned}

这里涉及矩阵 (u+Δu)(u+Δu)(\bold{u}^* + \Delta\bold{u})(\bold{u}^* + \Delta\bold{u})uu\bold{u}^* \bold{u}^* 的相减,由于:

(u+Δu)(u+Δu)=(ui+Δui)(uj+Δuj),uu=uiuj(\bold{u}^* + \Delta\bold{u})(\bold{u}^* + \Delta\bold{u}) = (u^*_{i} + \Delta u_i)(u^*_{j} + \Delta u_j), \quad \bold{u}^* \bold{u}^* = u^*_{i} u^*_{j}

其中 uiu_i^*Δui=Fiδt/ρ\Delta u_i = F_i \delta_{t} / \rho 分别为 u\bold{u}^*Δu\Delta\bold{u} 在 i 轴上的分量,所以:

(u+Δu)(u+Δu)uu=(ui+Δui)(uj+Δuj)uiuj=δtρ(uiFj+ujFi)+δt2ρ2FiFj=δtρ(ui+Fiδt2ρ)Fj+δtρ(uj+Fjδt2ρ)Fi\begin{aligned} (\bold{u}^* + \Delta\bold{u})(\bold{u}^* + \Delta\bold{u}) - \bold{u}^* \bold{u}^{*} &= (u^*_{i} + \Delta u_i)(u^*_{j} + \Delta u_j) - u^*_{i} u^*_{j} \\ &= \frac{\delta_t}{\rho} (u_i^* F_j + u_j^* F_i) + \frac{\delta_t^2}{\rho^2} F_i F_j \\ &= \frac{\delta_t}{\rho} (u_i^* + \frac{F_i \delta_t}{2 \rho}) F_j + \frac{\delta_t}{\rho} (u_j^* + \frac{F_j \delta_t}{2 \rho}) F_i \end{aligned}

这里令 vEDM=u+F2ρδt\bold{v}_{\rm{EDM}} = \bold{u}^{*} + \frac{\bold{F}}{2 \rho} \delta_{t} ,则 EDM 源项的展开式化简为:

Fα=δtwα[eαFcs2+12cs4(vEDMF+FvEDM):(eαeαcs2[I])](8)F_\alpha = \delta_t w_\alpha \left[ \frac{\bold{e}_\alpha \cdot \bold{F}}{c_s^2} + \frac{1}{2 c_s^4} \left( \bold{v}_{\rm{EDM}} \bold{F} + \bold{F} \bold{v}_{\rm{EDM}} \right) : (\bold{e}_\alpha \bold{e}_\alpha - c_s^2 [\bold{I}]) \right] \tag{8}

上式即为 EDM 源项的展开结果。

源项误差的 Chapman-Enskog 分析

这里的推导主要参考 Li 等[4:2]的文章,并补充了一些自己的笔记。

需要提醒的是,下文的速度记号和前文不同。

源项的各阶速度矩

根据 LBM 格子张量对称性,有前 5 阶表达式:

αwα=1,αwαeαi=0,αwαeαieαj=cs2δij,αwαeαieαjeαk=0αwαeαieαjeαkeαl=cs4(δijδkl+δikδjl+δilδkj)αwαeαieαjeαkeαleαm=0\sum_{\alpha} w_{\alpha} = 1 ,\quad \sum_{\alpha} w_{\alpha} e_{\alpha i} = 0 ,\\ \sum_{\alpha} w_{\alpha} e_{\alpha i} e_{\alpha j} = c_s^2 \delta_{ij} ,\quad \sum_{\alpha} w_{\alpha} e_{\alpha i} e_{\alpha j} e_{\alpha k} = 0 \\ \sum_{\alpha} w_{\alpha} e_{\alpha i} e_{\alpha j} e_{\alpha k} e_{\alpha l} = c_s^4 (\delta_{ij} \delta_{kl} + \delta_{ik} \delta_{jl} + \delta_{il} \delta_{kj}) \\ \sum_{\alpha} w_{\alpha} e_{\alpha i} e_{\alpha j} e_{\alpha k} e_{\alpha l} e_{\alpha m} = 0

其中 eαie_{\alpha i} 表示 D 维向量 eα\bold{e}_{\alpha} 的第 ii 个分量, wαw_\alphaeα\bold{e}_{\alpha} 的权重系数。 δij\delta_{ij} 为克罗内克符号。

所以,对于 EDM 格式的源项 Fα,EDMF_{\alpha,\mathrm{EDM}} ,其各阶速度矩为:

αFα,EDM=0,αeαFα,EDM=F,αeαeαFα,EDM=δt((uF+Fu)+δtFFρ)(9)\sum_{\alpha} F_{\alpha,\mathrm{EDM}} = 0 ,\quad \sum_{\alpha} \bold{e}_\alpha F_{\alpha,\mathrm{EDM}} = \bold{F} ,\quad\\ \sum_{\alpha} \bold{e}_\alpha \bold{e}_\alpha F_{\alpha,\mathrm{EDM}} = \delta_t \left( (\bold{u}^* \bold{F} + \bold{F}\bold{u}^*) + \delta_t \frac{\bold{FF}}{\rho} \right) \tag{9}

技术细节可见附录(A)。

LBM 的常规 Chapman-Enskog 展开

令展开参数 ϵ\epsilon 是与克努森数同阶的小量,则将分布函数展开为

fα=fα(0)+ϵfα(1)+ϵ2fα(2)+...,f_{\alpha} = f_{\alpha}^{(0)} + \epsilon f_{\alpha}^{(1)} + \epsilon^2 f_{\alpha}^{(2)} + ...,

源项展开为 Fα=ϵF1αF_{\alpha} = \epsilon F_{1 \alpha},时间和空间偏导展开为

t=ϵt1+ϵ2t2,x=ϵx1.\frac{\partial}{\partial t} = \epsilon \frac{\partial}{\partial t_1} + \epsilon^2 \frac{\partial}{\partial t_2} ,\quad \frac{\partial}{\partial \bold{x}} = \epsilon \frac{\partial}{\partial \bold{x}_1}.

将式(4)中的 fα(x+eαδt,t+δt)f_\alpha (\bold{x} + \bold{e}_\alpha \delta_t, t+\delta_t)fα(x,t)f_\alpha (\bold{x}, t) 处进行 Taylor 展开(至2阶项),并把上述展开式代入,可得 ϵ\epsilon 各阶项的方程为:

O(ϵ0):fα(0)=fα(eq),(101)O(ϵ1):D1αfα(0)=1τδtfα(1)+F1αδt,(102)O(ϵ2):fα(0)t2+D1αfα(1)+δt2D1α2fα(0)=1τδtfα(2).(103)\begin{aligned} O(\epsilon^0):\quad & f_{\alpha}^{(0)} = f_{\alpha}^{(eq)} , &(10-1)\\ O(\epsilon^1):\quad & \mathrm{D}_{1 \alpha} f_{\alpha}^{(0)} = -\frac{1}{\tau \delta_t} f_{\alpha}^{(1)} + \frac{F_{1 \alpha}}{\delta_t} , &(10-2)\\ O(\epsilon^2):\quad & \frac{\partial f_{\alpha}^{(0)}}{\partial t_2} + \mathrm{D}_{1 \alpha} f_{\alpha}^{(1)} + \frac{\delta_t}{2} \mathrm{D}_{1 \alpha}^2 f_{\alpha}^{(0)} = -\frac{1}{\tau \delta_t} f_{\alpha}^{(2)} . &(10-3)\\ \end{aligned}

其中 D1α=t1+eαx1\displaystyle \mathrm{D}_{1 \alpha} = \frac{\partial}{\partial t_1} + \bold{e}_{\alpha} \cdot \frac{\partial}{\partial \bold{x}_1}。将式(10-2)代入式(10-3)中,式(10-3)可被化简为式(10-4):

O(ϵ2):fα(0)t2+D1α(112τ)fα(1)+12D1αF1α=1τδtfα(2).(104)\begin{aligned} O(\epsilon^2):\quad & \frac{\partial f_{\alpha}^{(0)}}{\partial t_2} + \mathrm{D}_{1 \alpha} \left(1 - \frac{1}{2 \tau}\right) f_{\alpha}^{(1)} + \frac{1}{2} \mathrm{D}_{1 \alpha} F_{1 \alpha} = -\frac{1}{\tau \delta_t} f_{\alpha}^{(2)} . &(10-4) \end{aligned}

(1)考虑对式(10-3)和式(10-4)计算零阶矩,得:

ρt1+1(ρu)=0ρt2+121(δtF1)=0\frac{\partial \rho}{\partial t_1} + \nabla_1 \cdot (\rho \bold{u}^*) = 0 \\ \frac{\partial \rho}{\partial t_2} + \frac{1}{2} \nabla_1 \cdot (\delta_t \bold{F}_1) = 0 \\

此处 u=(ieαfα)/(ifα)\bold{u}^* = (\sum_{i} \bold{e}_\alpha f_\alpha) / (\sum_{i} f_\alpha) 并非真实流场速度,而 u^=u+Fδt/(2ρ)\hat{\bold{u}} = \bold{u}^* + \bold{F} \delta_t / (2 \rho) 为真实流场速度(也就是式(6)给出的形式)。

基于前面假设的偏微分关系式,我们可以得到 ρt+(ρu^)=0\displaystyle \frac{\partial \rho}{\partial t} + \nabla \cdot (\rho \hat{\bold{u}}) = 0

(2)同理,对式(10-3)和式(10-4)计算一阶矩,得:

ρut1+1(ρuu)=1p+F1ρut2+1[(112τ)αeαeαfα(1)]+δt2F1t1+121(αeαeαF1α)=0\frac{\partial \rho \bold{u}^*}{\partial t_1} + \nabla_1 \cdot (\rho \bold{u}^* \bold{u}^*) = -\nabla_1 p + \bold{F}_1 \\ \frac{\partial \rho \bold{u}^*}{\partial t_2} + \nabla_1 \cdot \left[\left(1 - \frac{1}{2 \tau}\right) \sum_{\alpha} \bold{e}_\alpha \bold{e}_\alpha f_{\alpha}^{(1)} \right] + \frac{\delta_t}{2} \frac{\partial \bold{F}_1}{\partial t_1} + \frac{1}{2} \nabla_1 \cdot \left( \sum_{\alpha} \bold{e}_\alpha \bold{e}_\alpha F_{1 \alpha} \right) = 0

其中 p=ρcs2p = \rho c_s^2

根据式(10-2),有:

αeαeαfα(1)=τ[δtt1(αeαeαfα(0))+δt1(αeαeαeαfα(0))αeαeαF1α]\begin{aligned} \sum_{\alpha} \bold{e}_\alpha \bold{e}_\alpha f_{\alpha}^{(1)} &= -\tau \left[ \delta_t \frac{\partial}{\partial t_1}\left( \sum_{\alpha} \bold{e}_\alpha \bold{e}_\alpha f_{\alpha}^{(0)} \right) \right. +\\ &\quad \left. \delta_t \nabla_1 \cdot \left( \sum_{\alpha} \bold{e}_\alpha \bold{e}_\alpha \bold{e}_\alpha f_{\alpha}^{(0)} \right) - \sum_{\alpha} \bold{e}_\alpha \bold{e}_\alpha F_{1 \alpha} \right] \end{aligned}

Π(1)=δt(τ12)[t1(αeαeαfα(0))+1(αeαeαeαfα(0))]=δt(τ12){ρcs2[1u+(1u)T]+uF1+F1u}\begin{aligned} \Pi^{(1)} &= -\delta_t \left( \tau - \frac{1}{2} \right) \left[ \frac{\partial}{\partial t_1}\left( \sum_{\alpha} \bold{e}_\alpha \bold{e}_\alpha f_{\alpha}^{(0)} \right) + \nabla_1 \cdot \left( \sum_{\alpha} \bold{e}_\alpha \bold{e}_\alpha \bold{e}_\alpha f_{\alpha}^{(0)} \right) \right] \\ &= -\delta_t \left( \tau - \frac{1}{2} \right) \{\rho c_s^2 [\nabla_1 \bold{u}^* + (\nabla_1 \bold{u}^*)^T] + \bold{u}^*\bold{F}_1 + \bold{F}_1 \bold{u}^* \} \end{aligned}

式(10-4)的一阶矩表示为: ρut2+1Π(1)+δt2F1t1+1(ταeαeαF1α)=0\displaystyle \frac{\partial \rho \bold{u}^*}{\partial t_2} + \nabla_1 \Pi^{(1)} + \frac{\delta_t}{2} \frac{\partial \bold{F}_1}{\partial t_1} + \nabla_1 \cdot \left( \tau \sum_{\alpha} \bold{e}_\alpha \bold{e}_\alpha F_{1 \alpha} \right) = 0

那么同样根据假设的微分关系,即可还原出一阶矩对应的方程。这里直接写出使用真实流场速度 u^=u+Fδt/(2ρ)\hat{\bold{u}} = \bold{u}^* + \bold{F} \delta_t / (2 \rho) 表示的形式:

(ρu^)t+(ρu^u^)=p+F+{ρν[1u+(1u)T}{ρν[1a+(1a)T]}+δt2ϵ2Ft2+[τδt(uF+Fu)+δt2FF4ρταeαeαFα]\begin{aligned} \frac{\partial (\rho \hat{\bold{u}})}{\partial t} + \nabla \cdot (\rho \hat{\bold{u}} \hat{\bold{u}}) &= -\nabla p + \bold{F} + \nabla \cdot \{ \rho \nu [\nabla_1 \bold{u}^* + (\nabla_1 \bold{u}^*)^T \} \\ &\quad - \nabla \cdot \{ \rho \nu [\nabla_1 \bold{a} + (\nabla_1 \bold{a})^T] \} + \frac{\delta_t}{2} \epsilon^2 \frac{\partial \bold{F}}{\partial t_2} \\ &\quad+ \nabla \cdot \left[ \tau \delta_t (\bold{u^* F} + \bold{F u^*}) + \delta_t^2 \frac{\bold{FF}}{4 \rho} - \tau \sum_{\alpha} \bold{e}_\alpha \bold{e}_\alpha F_{\alpha} \right] \end{aligned}

其中 a=δtF/2ρ\bold{a} = \delta_t \bold{F} / 2 \rhoν=(τ12)cs2δt\nu = (\tau - \frac{1}{2}) c_s^2 \delta_t 为流体运动粘度。 通过对比N-S方程,可见其误差项为:

Err={ρν[1a+(1a)T]}+δt2ϵ2Ft2+[τδt(uF+Fu)+δt2FF4ρταeαeαFα]\text{Err} = - \nabla \cdot \{ \rho \nu [\nabla_1 \bold{a} + (\nabla_1 \bold{a})^T] \} + \frac{\delta_t}{2} \epsilon^2 \frac{\partial \bold{F}}{\partial t_2} + \nabla \cdot \left[ \tau \delta_t (\bold{u^* F} + \bold{F u^*}) + \delta_t^2 \frac{\bold{FF}}{4 \rho} - \tau \sum_{\alpha} \bold{e}_\alpha \bold{e}_\alpha F_{\alpha} \right]

但上述的展开方式和Wagner等[5]使用Taylor展开的结果并不一致。 Li 等[4:3] 指出这种错误的来源是:上文将 fα(0)=fα(eq)(ρ,u)f_{\alpha}^{(0)} = f_{\alpha}^{(eq)}(\rho, \bold{u}^*),从而得到了 αeαfα(1)=0\sum_{\alpha} \bold{e}_{\alpha} f_{\alpha}^{(1)} = 0。 然而实际上 fα(0)=fα(eq)(ρ,u^)f_{\alpha}^{(0)} = f_{\alpha}^{(eq)}(\rho, \hat{\bold{u}}) ,从而有 αeαfα(1)=δtF1/2\sum_{\alpha} \bold{e}_{\alpha} f_{\alpha}^{(1)} = -\delta_t \bold{F}_1 / 2

修正后的 Chapman-Enskog 展开

因此,需要将原本的 LBE 等效地修改为:

fα(x+eαδt,t+δt)fα(x,t)=F^α1τ[fα(x,t)fα(eq)(ρ,u^)](11)f_\alpha (\bold{x} + \bold{e}_\alpha \delta_t, t+\delta_t) - f_\alpha (\bold{x}, t) = \hat{F}_{\alpha} -\frac{1}{\tau} \left[ f_\alpha (\bold{x}, t) - f_\alpha^{(eq)} (\rho, \hat{\bold{u}}) \right] \tag{11}

其中 F^α=Fα1τ(fα(eq)(ρ,u^)fα(eq)(ρ,u))\hat{F}_{\alpha} = F_{\alpha} - \frac{1}{\tau} (f_\alpha^{(eq)} (\rho, \hat{\bold{u}}) - f_\alpha^{(eq)} (\rho, \bold{u}^*)) 为基于原始源项 FαF_{\alpha} 修改而来的等效源项。并且需要强调的是,式(11)中的平衡态采用真实流场速度 u^\hat{\bold{u}} 计算。 在式(11)这一等效公式上,执行与上一节一致的 Chapman-Enskog 展开后,可得到还原的N-S方程为:

(ρu^)t+(ρu^u^)=p+F+{ρν[1u^+(1u^)T}+[(τ12)δt(u^F+Fu^)ταeαeαF^α](12)\begin{aligned} \frac{\partial (\rho \hat{\bold{u}})}{\partial t} + \nabla \cdot (\rho \hat{\bold{u}} \hat{\bold{u}}) &= -\nabla p + \bold{F} + \nabla \cdot \{ \rho \nu [\nabla_1 \hat{\bold{u}} + (\nabla_1 \hat{\bold{u}})^T \} \\ &\quad + \nabla \cdot \left[ \left(\tau - \frac{1}{2}\right) \delta_t (\hat{\bold{u}}\bold{F} + \bold{F}\hat{\bold{u}}) - \tau \sum_{\alpha} \bold{e}_\alpha \bold{e}_\alpha \hat{F}_{\alpha} \right] \end{aligned} \tag{12}

式(12)的误差项为:

Err=[(τ12)δt(u^F+Fu^)ταeαeαF^α](13)\text{Err} = \nabla \cdot \left[ \left(\tau - \frac{1}{2}\right) \delta_t (\hat{\bold{u}}\bold{F} + \bold{F}\hat{\bold{u}}) - \tau \sum_{\alpha} \bold{e}_\alpha \bold{e}_\alpha \hat{F}_{\alpha} \right] \tag{13}

将 EDM 的源项代入式(13)中,得到: Err=δt2(FF4ρ)\text{Err}=-\delta_t^2 \nabla\cdot\left( \frac{\bold{FF}}{4 \rho} \right)

附录

(A)源项各阶速度矩的推导

这里仅以 αeαeαFα,EDM\displaystyle \sum_{\alpha} \bold{e}_\alpha \bold{e}_\alpha F_{\alpha,\mathrm{EDM}} 的计算举例来简单说明。

αeαeαFα,EDM=αeαeαδtwα[eαFcs2+12cs4(vEDMF+FvEDM):(eαeαcs2[I])]=δtcs2α[eαeα(wαeαF)]+δt2cs4αwαeαeα[(vEDMF+FvEDM):(eαeαcs2[I])]\begin{aligned} \sum_{\alpha} \bold{e}_{\alpha} \bold{e}_{\alpha} F_{\alpha,\mathrm{EDM}} &= \sum_{\alpha} \bold{e}_\alpha \bold{e}_\alpha \cdot \delta_t w_\alpha \left[ \frac{\bold{e}_\alpha \cdot \bold{F}}{c_s^2} + \right.\\ &\quad\left. \frac{1}{2 c_s^4} \left( \bold{v}_{\rm{EDM}} \bold{F} + \bold{F} \bold{v}_{\rm{EDM}} \right) : (\bold{e}_\alpha \bold{e}_\alpha - c_s^2 [\bold{I}]) \right] \\ &= \frac{\delta_t}{c_s^2} \sum_{\alpha} \left[ \bold{e}_\alpha \bold{e}_\alpha (w_\alpha \bold{e}_\alpha \cdot \bold{F}) \right] + \\ &\quad \frac{\delta_t}{2 c_s^4} \sum_{\alpha} w_{\alpha} \bold{e}_\alpha \bold{e}_\alpha \cdot [\left( \bold{v}_{\rm{EDM}} \bold{F} + \bold{F} \bold{v}_{\rm{EDM}} \right) : (\bold{e}_\alpha \bold{e}_\alpha - c_s^2 [\bold{I}])] \end{aligned}

一方面,对于 α[eαeα(wαeαF)]\displaystyle \sum_{\alpha} \left[ \bold{e}_\alpha \bold{e}_\alpha (w_\alpha \bold{e}_\alpha \cdot \bold{F}) \right] 这个矩阵,它的第 ii 行第 jj 列写作

kFkα(wαeαieαjeαk)=kFk0=0\sum_{k} F_{k} \sum_{\alpha}(w_{\alpha} e_{\alpha i} e_{\alpha j} e_{\alpha k}) = \sum_{k} F_{k} \cdot 0 = 0

另一方面,已知 vEDM=u+F2ρδt\bold{v}_{\rm{EDM}} = \bold{u}^{*} + \frac{\bold{F}}{2 \rho} \delta_{t},由于 (vEDMF+FvEDM)\left( \bold{v}_{\rm{EDM}} \bold{F} + \bold{F} \bold{v}_{\rm{EDM}} \right) 为矩阵。所以,下文为方便起见,我们记

[B]=vEDMF+FvEDM=uF+Fu+δtρFF[\bold{\mathbb{B}}] = \bold{v}_{\rm{EDM}} \bold{F} + \bold{F} \bold{v}_{\rm{EDM}} = \bold{u}^{*} \bold{F} + \bold{F} \bold{u}^{*} + \frac{\delta_t}{\rho}\bold{F}\bold{F}

[B]:(eαeαcs2[I])[\bold{\mathbb{B}}] : (\bold{e}_\alpha \bold{e}_\alpha - c_s^2 [\bold{I}]) 是一个标量。
对于矩阵 [A]=αwαeαeα{[B]:(eαeαcs2[I])}\displaystyle [\bold{\mathbb{A}}] = \sum_{\alpha} w_{\alpha} \bold{e}_\alpha \bold{e}_\alpha \cdot \{[\bold{\mathbb{B}}] : (\bold{e}_\alpha \bold{e}_\alpha - c_s^2 [\bold{I}])\} ,它的第 ii 行第 jjAij\mathbb{A}_{ij} 写作

Aij=αwαeαieαj[klBkl(eαkeαlcs2δkl)]=klBklα{wαeαieαj(eαkeαlcs2δkl)}=klBklcs4(δilδjk+δikδjl)=(Bij+Bji)cs4\begin{aligned} \mathbb{A}_{ij} &= \sum_{\alpha} w_{\alpha} e_{\alpha i} e_{\alpha j} \left[ \sum_{k} \sum_{l} \mathbb{B}_{kl} (e_{\alpha k} e_{\alpha l} - c_s^2 \delta_{kl}) \right] \\&= \sum_{k} \sum_{l} \mathbb{B}_{kl} \sum_{\alpha} \left\{ w_{\alpha} e_{\alpha i} e_{\alpha j} (e_{\alpha k} e_{\alpha l} - c_s^2 \delta_{kl}) \right\} \\&= \sum_{k} \sum_{l} \mathbb{B}_{kl} \cdot c_s^4 (\delta_{il} \delta_{jk} + \delta_{ik} \delta_{jl}) \\&= (\mathbb{B}_{ij} +\mathbb{B}_{ji}) c_s^4 \end{aligned}

因为 [B][\mathbb{B}] 是对称矩阵,所以 Aij=2cs4Bij\mathbb{A}_{ij} =2 c_s^4 \mathbb{B}_{ij}。也就有:

αeαeαFα,EDM=0+δt2cs4αwαeαeα[(vEDMF+FvEDM):(eαeαcs2[I])]=δt(vEDMF+FvEDM)=δt(uF+Fu+δtρFF)\begin{aligned} \sum_{\alpha} \bold{e}_\alpha \bold{e}_\alpha F_{\alpha,\mathrm{EDM}} &= \vec{\bold{0}} + \frac{\delta_t}{2 c_s^4} \sum_{\alpha} w_{\alpha} \bold{e}_\alpha \bold{e}_\alpha \cdot [\left( \bold{v}_{\rm{EDM}} \bold{F} + \bold{F} \bold{v}_{\rm{EDM}} \right) : (\bold{e}_\alpha \bold{e}_\alpha - c_s^2 [\bold{I}])] \\&= \delta_t \left( \bold{v}_{\rm{EDM}} \bold{F} + \bold{F} \bold{v}_{\rm{EDM}} \right) \\&= \delta_t \left( \bold{u}^{*} \bold{F} + \bold{F} \bold{u}^{*} + \frac{\delta_t}{\rho}\bold{F}\bold{F} \right) \end{aligned}

综上, αeαeαFα,EDM=δt(uF+Fu+δtFFρ)\displaystyle \sum_{\alpha} \bold{e}_\alpha \bold{e}_\alpha F_{\alpha,\mathrm{EDM}} = \delta_t \left( \bold{u}^* \bold{F} + \bold{F}\bold{u}^* + \delta_t \frac{\bold{FF}}{\rho} \right) 成立。其他低阶矩均采用类似方法进行计算。当然,这也同样可以拓展至其他源项的速度矩计算。

(B)修正源项的计算

由于 a=δtF/2ρ=u^u\bold{a} = \delta_t \bold{F} / 2 \rho = \hat{\bold{u}} - \bold{u}^* ,则 ρa=δtF/2\rho \bold{a} = \delta_t \bold{F} / 2 。因此:

1τ(fα(eq)(ρ,u^)fα(eq)(ρ,u))=ρwατ[eαacs2+12cs4(u^u^uu):(eαeαcs2[I])]=ρwατ[eαacs2+12cs4(ua+au+aa):(eαeαcs2[I])]=wαδtτ[eαF2cs2+12cs4(12(uF+Fu)+δtFF4ρ):(eαeαcs2[I])]\begin{aligned} & \frac{1}{\tau} (f_\alpha^{(eq)} (\rho, \hat{\bold{u}}) - f_\alpha^{(eq)} (\rho, \bold{u}^*)) \\=& \frac{\rho w_{\alpha}}{\tau} \left[ \frac{\bold{e}_{\alpha} \cdot \bold{a}}{c_s^2} + \frac{1}{2 c_s^4} (\hat{\bold{u}}\hat{\bold{u}} - \bold{u^* u^*}):(\bold{e}_\alpha \bold{e}_\alpha - c_s^2 [\bold{I}]) \right] \\=& \frac{\rho w_{\alpha}}{\tau} \left[ \frac{\bold{e}_{\alpha} \cdot \bold{a}}{c_s^2} + \frac{1}{2 c_s^4} ( \bold{u^* a} + \bold{a u^*} + \bold{aa}):(\bold{e}_\alpha \bold{e}_\alpha - c_s^2 [\bold{I}]) \right] \\=& \frac{w_{\alpha} \delta_t}{\tau} \left[ \frac{\bold{e}_{\alpha} \cdot \bold{F}}{2 c_s^2} + \frac{1}{2 c_s^4} \left( \frac{1}{2} (\bold{u^* F} + \bold{F u^*}) + \delta_t \frac{\bold{FF}}{4 \rho} \right) : (\bold{e}_\alpha \bold{e}_\alpha - c_s^2 [\bold{I}]) \right] \end{aligned}

由于 EDM 源项的表达式为:

Fα,EDM=δtwα[eαFcs2+12cs4(u^F+Fu^):(eαeαcs2[I])]F_{\alpha,\mathrm{EDM}} = \delta_t w_\alpha \left[ \frac{\bold{e}_\alpha \cdot \bold{F}}{c_s^2} + \frac{1}{2 c_s^4} \left( \hat{\bold{u}} \bold{F} + \bold{F} \hat{\bold{u}} \right) : (\bold{e}_\alpha \bold{e}_\alpha - c_s^2 [\bold{I}]) \right]

因此,其对应修正源项为

Fα,EDM1τ(fα(eq)(ρ,u^)fα(eq)(ρ,u))=eαFcs2(112τ)+wαδt2cs4{[(12τ1)(uF+Fu)(aF+Fa)δt4ρτFF]:(eαeαcs2[I])}\begin{aligned} & F_{\alpha,\mathrm{EDM}} - \frac{1}{\tau} (f_\alpha^{(eq)} (\rho, \hat{\bold{u}}) - f_\alpha^{(eq)} (\rho, \bold{u}^*)) \\=& \frac{\bold{e}_\alpha \cdot \bold{F}}{c_s^2} (1 - \frac{1}{2 \tau}) + \\& \frac{w_{\alpha} \delta_t}{2 c_s^4} \left\{ \left[ (\frac{1}{2 \tau} - 1) (\bold{u^* F} + \bold{F u^*}) - (\bold{a F} + \bold{F a}) \right.\right. \\& \left.\left. - \frac{\delta_t}{4 \rho \tau} \bold{FF} \right] : (\bold{e}_\alpha \bold{e}_\alpha - c_s^2 [\bold{I}]) \right\} \end{aligned}


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