沉了么。。?有大佬试试我的算例了么?
RebelYoung
帖子
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rhoCentralFoam发散,出现Negative Initial Temperature -
rhoCentralFoam发散,出现Negative Initial Temperature
250m/s的cube,60步出现negative initial temperature。# Field minima and maxima # Time field min location(min) max location(max) 3.57143e-05 T 1.454278e+02 (1.646393e-02 1.393888e-19 -1.709886e-18) 3.108947e+02 (-1.646393e-02 1.393888e-19 -1.725321e-18) 3.57143e-05 e 1.043157e+05 (1.646393e-02 1.393888e-19 -1.709886e-18) 2.230054e+05 (-1.646393e-02 1.393888e-19 -1.725321e-18) 3.64286e-05 T 1.335562e+02 (5.517241e-03 1.105814e-02 1.105814e-02) 3.098790e+02 (-1.646393e-02 1.393888e-19 -1.725321e-18) 3.64286e-05 e 9.580017e+04 (5.517241e-03 1.105814e-02 1.105814e-02) 2.222768e+05 (-1.646393e-02 1.393888e-19 -1.725321e-18) 3.71429e-05 T 2.917792e+01 (6.206897e-03 1.105814e-02 1.105814e-02) 3.078215e+02 (-1.646393e-02 1.393888e-19 -1.725321e-18) 3.71429e-05 e 2.092939e+04 (6.206897e-03 1.105814e-02 1.105814e-02) 2.208010e+05 (-1.646393e-02 1.393888e-19 -1.725321e-18) 3.58333e-05 T 1.400088e+02 (5.517241e-03 1.105814e-02 1.179091e-02) 3.108729e+02 (-1.646393e-02 1.393888e-19 -1.725321e-18) 3.58333e-05 e 1.004286e+05 (5.517241e-03 1.105814e-02 1.179091e-02) 2.229898e+05 (-1.646393e-02 1.393888e-19 -1.725321e-18) 3.65278e-05 T 6.218740e+01 (5.517241e-03 1.105814e-02 1.105814e-02) 3.097428e+02 (-1.646393e-02 1.393888e-19 -1.725321e-18) 3.65278e-05 e 4.460715e+04 (5.517241e-03 1.105814e-02 1.105814e-02) 2.221792e+05 (-1.646393e-02 1.393888e-19 -1.725321e-18)
最后几步的温度最值,最后两步$T_{min}$下降一个量级。
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rhoCentralFoam发散,出现Negative Initial Temperature@东岳 我是用pointwise画了导出的,这个球比较难画 ,
我的另一个简单算例cube (提取码: ywvc)是有附面层的全结构网格,上传的设置是初始条件是类似rhoS的0012算例的freestream type。
来流速度30m/s,就是上面贴图的龟派气功的结果,在几百步后也会发散,出现负温度。 -
rhoCentralFoam发散,出现Negative Initial Temperature@东岳 重新试了一下250m/s,相当于0.83Ma,算了20步就出现负初始温度的问题
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rhoCentralFoam发散,出现Negative Initial Temperaturehttps://www.cfd-china.com/topic/1737/可压缩求解器为什么密度残差一直为0-迭代步也一直是0
这里面回答了rho,rhoE,rhoU残差为0的原因。
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rhoCentralFoam发散,出现Negative Initial Temperature@东岳 那么高速导致雷诺数量级太大,层流模型还能算么?
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rhoCentralFoam发散,出现Negative Initial Temperature@东岳 我其他的边界条件pT都是一样的,控制雷诺数,计算了不同的速度。因为是层流,所以上传的是最小速度1m/s的。
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rhoCentralFoam发散,出现Negative Initial Temperature@东岳 是的哇
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rhoCentralFoam发散,出现Negative Initial Temperature尝试画粗网格计算正方体外流,结果确实可以计算,deltat=10^-7算到0.05s,未出现以上问题。
对应精细网格,计算到300个时间步,又出现了温度陡增的发散问题。
细网格内能残差
粗网格内能残差两个算例的迭代中能量残差都是initial residual< final residual,不过粗网格没有发散。
在这些rhoC算例中计算发现,温度压强都有“龟派气功”的特效。。。前缘驻点附近形成的高压会脱体。。。后缘驻点类似。。。
到最后消失了。。。 -
rhoCentralFoam发散,出现Negative Initial Temperature算例文件在文中已经贴出
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rhoCentralFoam发散,出现Negative Initial Temperature计算目的:计算跨声速外流,先尝试简单模型计算,尝试使用rhoCentralFoam求解器。
算例外形 球 直径 0.002m。 边界条件 自由流 来流速度 1到250m/s均有计算 压强 6.0e4 Pa 温度 270K 流体类型 标准气体 网格为非结构,prism附面层。
条件根据rhoC的tutorials算例修改。首先说一下在rhoC的tutorials算例发现的几个现象:
- 所有rhoC的tutorials算例均为laminar。
- 所有rhoC的tutorials算例计算中输出的:
diagonal: Solving for rho, Initial residual = 0, Final residual = 0, No Iterations 0 diagonal: Solving for rhoUx, Initial residual = 0, Final residual = 0, No Iterations 0 diagonal: Solving for rhoUy, Initial residual = 0, Final residual = 0, No Iterations 0 diagonal: Solving for rhoE, Initial residual = 0, Final residual = 0, No Iterations 0
残差始终为0。和我计算中一致,不知道这是什么问题。
3. 有些算例为了控制Mach数,速度温度都设置的很低,看似是低速但是马赫数很高。但是这些算例中的rho/rhoU/rhoE的残差也始终是0。rcf_sphere算例(提取码: b7h6)出现的问题:Negative Initial Temperature
报错如下:
--> FOAM FATAL ERROR: Negative initial temperature T0: -10272.9 From function Foam::scalar Foam::species::thermo<Thermo, Type>::T(Foam::scalar, Foam::scalar, Foam::scalar, Foam::scalar (Foam::species::thermo<Thermo, Type>::*)(Foam::scalar, Foam::scalar) const, Foam::scalar (Foam::species::thermo<Thermo, Type>::*)(Foam::scalar, Foam::scalar) const, Foam::scalar (Foam::species::thermo<Thermo, Type>::*)(Foam::scalar) const, bool) const [with Thermo = Foam::hConstThermo<Foam::perfectGas<Foam::specie> >; Type = Foam::sensibleInternalEnergy; Foam::scalar = double; Foam::species::thermo<Thermo, Type> = Foam::species::thermo<Foam::hConstThermo<Foam::perfectGas<Foam::specie> >, Foam::sensibleInternalEnergy>] in file /home/rebel/OpenFOAM/OpenFOAM-7/src/thermophysicalModels/specie/lnInclude/thermoI.H at line 56. FOAM aborting #0 Foam::error::printStack(Foam::Ostream&) at ??:? #1 Foam::error::abort() at ??:? #2 Foam::species::thermo<Foam::hConstThermo<Foam::perfectGas<Foam::specie> >, Foam::sensibleInternalEnergy>::T(double, double, double, double (Foam::species::thermo<Foam::hConstThermo<Foam::perfectGas<Foam::specie> >, Foam::sensibleInternalEnergy>::*)(double, double) const, double (Foam::species::thermo<Foam::hConstThermo<Foam::perfectGas<Foam::specie> >, Foam::sensibleInternalEnergy>::*)(double, double) const, double (Foam::species::thermo<Foam::hConstThermo<Foam::perfectGas<Foam::specie> >, Foam::sensibleInternalEnergy>::*)(double) const, bool) const at ??:? #3 Foam::hePsiThermo<Foam::psiThermo, Foam::pureMixture<Foam::constTransport<Foam::species::thermo<Foam::hConstThermo<Foam::perfectGas<Foam::specie> >, Foam::sensibleInternalEnergy> > > >::calculate() at ??:? #4 Foam::hePsiThermo<Foam::psiThermo, Foam::pureMixture<Foam::constTransport<Foam::species::thermo<Foam::hConstThermo<Foam::perfectGas<Foam::specie> >, Foam::sensibleInternalEnergy> > > >::correct() at ??:? #5 ? in "/home/rebel/OpenFOAM/OpenFOAM-7/platforms/linux64GccDPInt32Opt/bin/rhoCentralFoam" #6 __libc_start_main in "/lib/x86_64-linux-gnu/libc.so.6" #7 ? in "/home/rebel/OpenFOAM/OpenFOAM-7/platforms/linux64GccDPInt32Opt/bin/rhoCentralFoam"
该错误往往发生在计算几十到一百个时间步后出现,根据残差可以发现和算例的区别是,每步的initial residuals都比final residuals大,而tutorials算例都是减小的,符合收敛的趋势。
但是,奇怪的是每一步的初始残差又总是只有10^-7^量级,也并不是很大。迭代后往往上升两个量级。。
其中内能e的上升比较明显,能从10^-9^上升到10^-5^。
所以光看残差趋势是预想不到某一步的直接发散。之后增加minMax函数监视,发现在接近发散的几个时间步,最大内能和温度都会陡增。从约200K增加到2000多K。
但是由于时间步长太短,几十步发散的情况下,可视化后处理看不出什么道道。球表面像长痘痘一样出现一些高温点。这是说明附面层网格出毛病了??
总的来说,应该就是能量方程发散,出现非物理的内能/温度。另外,fvOptions限制器已经加了,不过没起作用。。。。
请问这个负初始温度到底是啥?以及解决办法。
谢谢谢!
还有两个小个问题是,
1.上面报错的一堆“#::???” ,这堆报错信息到底能看出啥呀?这里面的问号是我电脑乱码了吗?
2.为什么同样laminar,同样的求解器,在不同算例里fvsolution中设置的量不同呢?
我是根据obliqueShock算例修改的,只是改了polyMesh和0文件下边界条件。可是运行报错e未定义,但是原算例本来就没有哇。 -
可压流计算发散,出现Negative Initial Temperature 问题如何处理?最新看到的说法是,T估算值或者插值中出现了问题。比如方程解的是h,那么从h=cp(T)T中解出T的估算值,结果是负的。。
rhoC解的是e,那么e=CvT,cv基本不变,那应该是e出现负值导致T出现负值。。。 -
可压流计算发散,出现Negative Initial Temperature 问题如何处理?@bestucan 可是上面minMax监视的全场温度,并没有出现负温度啊?初始值220K,最低也就210.。。
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可压流计算发散,出现Negative Initial Temperature 问题如何处理?以上基本描述的都是rhoCentralFoam问题,报错是Negative Initial Temperature,但是全场最小温度并没有负值。。
这个rcf_sphere_laminar是根据,$FOAM_TUTORIALS/compressible/rhoCentralFoam/obliqueShock改的。是层流计算,/0下设置了p,T,U三个量。
以下贴出rhoC 0下文件:
./0/pFoamFile { version 2.0; format ascii; class volScalarField; object p; } // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // dimensions [1 -1 -2 0 0 0 0]; internalField uniform 100000; boundaryField { ball { type zeroGradient; } inlet { type zeroGradient; } outlet { type fixedValue; value uniform 100000; } far { type zeroGradient; } }
./0/T
FoamFile { version 2.0; format ascii; class volScalarField; object T; } // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // dimensions [0 0 0 1 0 0 0]; internalField uniform 270; boundaryField { ball { type zeroGradient; } inlet { type fixedValue; value uniform 270; } outlet { type zeroGradient; } far { type fixedValue; value uniform 270; } }
./0/U
其中U从1到250,都算过。都出现能量方程发散或negative initial temperature问题。FoamFile { version 2.0; format ascii; class volVectorField; object U; } // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // dimensions [0 1 -1 0 0 0 0]; internalField uniform (1 0 0); boundaryField { ball { type noSlip; } inlet { type fixedValue; value uniform (1 0 0); } outlet { type zeroGradient; } far { type fixedValue; value uniform (1 0 0); } }
checkMesh结果:
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // Create time Create polyMesh for time = 0 Time = 0 Mesh stats points: 28680 faces: 309924 internal faces: 293684 cells: 150902 faces per cell: 4 boundary patches: 4 point zones: 0 face zones: 0 cell zones: 0 Overall number of cells of each type: hexahedra: 0 prisms: 0 wedges: 0 pyramids: 0 tet wedges: 0 tetrahedra: 150902 polyhedra: 0 Checking topology... Boundary definition OK. Cell to face addressing OK. Point usage OK. Upper triangular ordering OK. Face vertices OK. Number of regions: 1 (OK). Checking patch topology for multiply connected surfaces... Patch Faces Points Surface topology ball 9780 4892 ok (closed singly connected) far 4404 2278 ok (non-closed singly connected) inlet 1028 553 ok (non-closed singly connected) outlet 1028 553 ok (non-closed singly connected) Checking geometry... Overall domain bounding box (-0.1 -0.1 -0.1) (0.1 0.1 0.1) Mesh has 3 geometric (non-empty/wedge) directions (1 1 1) Mesh has 3 solution (non-empty) directions (1 1 1) Boundary openness (1.54762e-16 -1.49987e-17 -1.09064e-16) OK. Max cell openness = 3.03063e-16 OK. Max aspect ratio = 5.29154 OK. Minimum face area = 3.38388e-08. Maximum face area = 0.000137468. Face area magnitudes OK. Min volume = 4.46514e-12. Max volume = 4.98913e-07. Total volume = 0.00799582. Cell volumes OK. Mesh non-orthogonality Max: 58.0988 average: 22.4508 Non-orthogonality check OK. Face pyramids OK. Max skewness = 0.67456 OK. Coupled point location match (average 0) OK. Mesh OK. End
./constant/thermophysicalProperties: 此文件根据rhoS中计算翼型的文件修改,因为原算例是想控制mach数等原因,改的不符合物理性质,且mu=0。我将其改成了正常参数。
FoamFile { version 2.0; format ascii; class dictionary; location "constant"; object thermophysicalProperties; } // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // thermoType { type hePsiThermo; mixture pureMixture; transport const; thermo hConst; equationOfState perfectGas; specie specie; energy sensibleInternalEnergy; } mixture { // normalised gas specie { molWeight 28.9; } thermodynamics { Cp 1005; Hf 0; } transport { mu 1.8e-5; Pr 0.71; } }
FoamFile { version 2.0; format ascii; class dictionary; location "constant"; object turbulenceProperties; } // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // simulationType laminar;
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可压流计算发散,出现Negative Initial Temperature 问题如何处理?@sibo 上面传了个rcf_sphere_laminar 的压缩文件,里面有polyMesh 以外的文件。BCs 的话真的很简单,上面描述过了。
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可压流计算发散,出现Negative Initial Temperature 问题如何处理?@sibo log是rhoC 的,算例thermo 中mu 1.82E -5,肯定是viscous 哇。
一开始我算的超过0.3Ma ,很快发散。我怀疑是雷诺数太高的层流问题。。。就把速度改小了,雷诺数在10的3次方量级。 -
可压流计算发散,出现Negative Initial Temperature 问题如何处理?log.zip
上传一个log文件。。。 -
可压流计算发散,出现Negative Initial Temperature 问题如何处理?观察输出的迭代信息,发现,U rhoU rhoE三个值始终残差为0,我以为是不需要设置求解的,尝试在fvsolution中注销掉了,发现计算运行时会报错,说这几个量没有定义。。。定义了好像又不求解。。这是怎么回事呢?
而且我rcf迭代中,final残差总是比final残差大。。几个量级。。
并发现,上一步的final并不是下一步的initial残差。这是怎么回事呀?
初始残差一般都是10的-7量级,怎么迭代后越来越大,但是下一步的初始残差还是e-7。。。 要被虐哭了,大佬帮帮我。deltaT = 8.38392e-08 Mean and max Courant Numbers = 0.010868 0.525071 Time = 4.93006e-07 diagonal: Solving for rho, Initial residual = 0, Final residual = 0, No Iterations 0 diagonal: Solving for rhoUx, Initial residual = 0, Final residual = 0, No Iterations 0 diagonal: Solving for rhoUy, Initial residual = 0, Final residual = 0, No Iterations 0 diagonal: Solving for rhoUz, Initial residual = 0, Final residual = 0, No Iterations 0 smoothSolver: Solving for Ux, Initial residual = 6.98094e-07, Final residual = 3.53286e-05, No Iterations 1000 smoothSolver: Solving for Uy, Initial residual = 6.01407e-06, Final residual = 5.40888e-05, No Iterations 1000 smoothSolver: Solving for Uz, Initial residual = 2.91948e-06, Final residual = 2.84312e-05, No Iterations 1000 diagonal: Solving for rhoE, Initial residual = 0, Final residual = 0, No Iterations 0 smoothSolver: Solving for e, Initial residual = 7.3214e-08, Final residual = 0.000463259, No Iterations 1000 ExecutionTime = 48.36 s ClockTime = 54 s
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可压流计算发散,出现Negative Initial Temperature 问题如何处理?rcf_sphere_laminar.zip
@sibo 这里面差个polyMesh,那个文件有点大。 -
可压流计算发散,出现Negative Initial Temperature 问题如何处理?残差监视,也没有过高量级的残差。。。
# Residuals # Time rho Ux Uy Uz rhoUx rhoUy rhoUz e rhoE 1.2e-07 0.000000e+00 9.999998e-01 9.999987e-01 9.999987e-01 0.000000e+00 0.000000e+00 0.000000e+00 7.969064e-06 0.000000e+00 2.20464e-07 0.000000e+00 2.111891e-06 1.380125e-05 4.022545e-06 0.000000e+00 0.000000e+00 0.000000e+00 1.313458e-07 0.000000e+00 3.19452e-07 0.000000e+00 1.264645e-06 1.060253e-05 3.560864e-06 0.000000e+00 0.000000e+00 0.000000e+00 1.072603e-07 0.000000e+00 4.09167e-07 0.000000e+00 8.909982e-07 7.791157e-06 3.130739e-06 0.000000e+00 0.000000e+00 0.000000e+00 8.653875e-08 0.000000e+00 4.93006e-07 0.000000e+00 6.980943e-07 6.014070e-06 2.919484e-06 0.000000e+00 0.000000e+00 0.000000e+00 7.321404e-08 0.000000e+00 5.72842e-07 0.000000e+00 5.830812e-07 4.767039e-06 2.802532e-06 0.000000e+00 0.000000e+00 0.000000e+00 6.407240e-08 0.000000e+00 6.49727e-07 0.000000e+00 5.076418e-07 3.877868e-06 2.757184e-06 0.000000e+00 0.000000e+00 0.000000e+00 5.741409e-08 0.000000e+00 7.24235e-07 0.000000e+00 4.533701e-07 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