请问有人在of中成功使用动态增厚火焰模型吗
yuky
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有人用过动态增厚火焰模型吗 -
重新编译热物理库请问您成功了吗,我也有这方面的需要
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对于拉乌尔喷管构型(出口超声速)进行气相燃料燃烧仿真用reactingfoam合适吗以及对于入口气态氧化剂超声速射入燃烧室,入口液态燃料低速进入燃烧室进行非预混燃烧,最后速度为低马赫数的用sprayFoam进行燃烧仿真合适吗
请各位给小白点建议 -
OpenFOAM的两个燃烧求解器@cccrrryyy 我想请问一下您对这个“如果采用低马赫数近似,密度随压力不变,那是不是就相当于认为声速无穷大?这样假设会导致什么呢?”有个结论了吗,对于发动机来说,燃料进入燃烧室通常是速度较快的,但燃料开始燃烧之后速度又是正常低马赫数,请问这种用reactingFoam合适吗
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关于Ansys三维流体域网格导入openfoam的问题同问,我也出现了这个问题,不知道该不该去调整
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一个关于 Axisymmetric Subsonic Jet 的问题@King_RVM 方便问您一些具体的网格导入和修改边界条件的细节吗,因为我现在导入网格改边界条件总是失败
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一个关于 Axisymmetric Subsonic Jet 的问题求问大佬如何绘制楔形模型的,是在icem里画完了导入openfoam的嘛,再改的wedge的边界条件嘛,我是要算一个轴对称圆柱燃烧室
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求问ICEM中的楔形网格导入openfoam之后壁面条件如何修改@李东岳 好的,非常感谢东岳老师
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求问ICEM中的楔形网格导入openfoam之后壁面条件如何修改原模型是圆柱燃烧室,为了简化计算只画了1/12的部分
我个人想法是将两个面改为wedge,但是checkMesh的时候发现识别不了,会报错,求大神指教报错如下:
Checking geometry...
Overall domain bounding box (0 -6.363451432e-19 -1.169089492e-12) (0.2372166655 0.01928534508 0.009642672539)
Mesh has 2 geometric (non-empty/wedge) directions (1 1 0)
Mesh has 3 solution (non-empty) directions (1 1 1)
Wedge WALL_RANSHAOSHI2 with angle 0 degrees
***Cannot find opposite wedge for wedge WALL_RANSHAOSHI2
Boundary openness (-1.075387266e-17 -1.69211467e-15 -1.2396473e-14) OK.
Max cell openness = 4.03570353e-16 OK.
Max aspect ratio = 7.562500293 OK.
Minimum face area = 4.890642405e-09. Maximum face area = 2.500000033e-07. Face area magnitudes OK.
Min volume = 6.010518271e-13. Max volume = 9.284234891e-11. Total volume = 1.511515734e-05. Cell volumes OK.
Mesh non-orthogonality Max: 63.85295712 average: 15.3592327
Non-orthogonality check OK.
Face pyramids OK.
Max skewness = 0.8283279386 OK.
Coupled point location match (average 0) OK.Failed 1 mesh checks.
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reactingFoam修改化学反应机理后遇到了问题又又又遇到了新问题,一步都没算下去,请问这种问题一般出在哪里
Create timeCreate mesh for time = 0
PIMPLE: No convergence criteria found
PIMPLE: Operating solver in transient mode with 1 outer corrector
PIMPLE: Operating solver in PISO modeUsing LTS
Reading thermophysical propertiesSelecting thermodynamics package
{
type heRhoThermo;
mixture multiComponentMixture;
transport sutherland;
thermo janaf;
energy sensibleEnthalpy;
equationOfState perfectGas;
specie specie;
}Reading field U
Reading/calculating face flux field phi
Creating turbulence model.
Selecting turbulence model type RAS
Selecting RAS turbulence model kEpsilon
kEpsilonCoeffs
{
Prt 0.85;
Cmu 0.09;
C1 1.44;
C2 1.92;
C3 0;
sigmak 1;
sigmaEps 1.3;
}Creating thermophysical transport model
Selecting thermophysical transport type RAS
Selecting default RAS thermophysical transport model unityLewisEddyDiffusivity
Creating reaction modelSelecting combustion model EDC
Selecting chemistry solver
{
solver ode;
method standard;
}standardChemistryModel: Number of species = 544 and reactions = 2446
Selecting ODE solver seulex
Creating field dpdtCreating field kinetic energy K
No MRF models present
No fvModels present
No fvConstraints presentStarting time loop
Time scales min/max:
Flow = 9.728569846e-08, 0.0001
Temperature = 4.494232837e+307, 4.494232837e+307
Composition = 4.494232837e+307, 4.494232837e+307
Overall = 9.728569846e-08, 0.0001
Time = 1e-07diagonal: Solving for rho, Initial residual = 0, Final residual = 0, No Iterations 0
DILUPBiCGStab: Solving for Ux, Initial residual = 1, Final residual = 0.0001092756986, No Iterations 1
DILUPBiCGStab: Solving for Uy, Initial residual = 1, Final residual = 0.006862564884, No Iterations 1
DILUPBiCGStab: Solving for Uz, Initial residual = 1, Final residual = 0.0001167898495, No Iterations 1
#0 Foam::error::printStack(Foam::Ostream&) at ??:?
#1 Foam::sigFpe::sigHandler(int) at ??:?
#2 ? in "/lib/x86_64-linux-gnu/libc.so.6"
#3 double Foam::standardChemistryModel<Foam::sutherlandTransport<Foam::species::thermo<Foam::janafThermo<Foam::perfectGasFoam::specie >, Foam::sensibleEnthalpy> > >::solve<Foam::Field<double> >(Foam::Field<double> const&) at ??:?
#4 Foam::combustionModels::EDC::correct() at ??:?
#5 ? in "/opt/openfoam9/platforms/linux64GccDPInt32Opt/bin/reactingFoam"
#6 ? in "/lib/x86_64-linux-gnu/libc.so.6"
#7 __libc_start_main in "/lib/x86_64-linux-gnu/libc.so.6"
#8 ? in "/opt/openfoam9/platforms/linux64GccDPInt32Opt/bin/reactingFoam"
Floating point exception (core dumped) -
reactingFoam报错@李东岳 是的东岳老师,发散的原因还在寻找,目前找到一个原因是有可能是我把出口当成壁面了,给的出口压力边界条件zeroGradient 所以压力出不去
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openFoam如何调用热物理库中的气体@vbcwl 请问你调用成功了嘛,我也在尝试firefoam的这里,我想改成正庚烷的
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reactingFoam报错好巧我也是!!跑了好几天然后出来浮点数溢出的报错,我的问题好像是压力一直无法收敛,一直再增长,这是我的部分报错,可以一起交流一下,我小白一只也在搞reactingfoam
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请问ReactingFoam可否用于气液两相燃烧计算@bestucan 好的好的,十分感谢!
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reactingFoam修改化学反应机理后遇到了问题@李东岳 好的,谢谢东岳老师,我去看看
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reactingFoam修改化学反应机理后遇到了问题这个问题解决了,但是出现了新的问题
No MRF models present No fvModels present No fvConstraints present #0 Foam::error::printStack(Foam::Ostream&) at ??:? #1 Foam::sigFpe::sigHandler(int) at ??:? #2 ? in "/lib/x86_64-linux-gnu/libc.so.6" #3 Foam::nutkWallFunctionFvPatchScalarField::nut() const at ??:? #4 Foam::nutWallFunctionFvPatchScalarField::updateCoeffs() at ??:? #5 Foam::GeometricField<double, Foam::fvPatchField, Foam::volMesh>::Boundary::evaluate() in "/opt/openfoam9/platforms/linux64GccDPInt32Opt/bin/reactingFoam" #6 Foam::RASModels::kEpsilon<Foam::CompressibleMomentumTransportModel<Foam::dynamicTransportModel> >::correctNut() at ??:? #7 ? in "/opt/openfoam9/platforms/linux64GccDPInt32Opt/bin/reactingFoam" #8 ? in "/lib/x86_64-linux-gnu/libc.so.6" #9 __libc_start_main in "/lib/x86_64-linux-gnu/libc.so.6" #10 ? in "/opt/openfoam9/platforms/linux64GccDPInt32Opt/bin/reactingFoam" Floating point exception (core dumped)
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reactingFoam修改化学反应机理后遇到了问题目前研一刚入门阶段,针对reactingfoam进行一些改动,用的是自己的构型,边界条件也相应做了一些调整,原本的参考案例是用CH4,我自己改成了C7H16,也把化学机理加了进来,现在遇到了这个问题不知道怎么办(报错如下所附),请求各位大神指点一下
--> FOAM FATAL ERROR: Sum of mass fractions is zero for species 544 ( 各种组分 ) From function void Foam::basicSpecieMixture::correctMassFractions() in file mixtures/basicSpecieMixture/basicSpecieMixture.C at line 205. FOAM exiting
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reactingFoam计算速度的问题@香柏树 请问你用ReactingFoam ras改les成功了吗,想和您请教一下
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用rhoReactingFoam对燃烧瞬态过程进行求解@myheart 好的好的,十分感谢,我再去研究一下
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请问ReactingFoam可否用于气液两相燃烧计算一枚小白,请问有用过reactingfoam的大佬吗,有很多问题都想请教一下