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yuky

@yuky
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最新

  • 有人用过动态增厚火焰模型吗
    Y yuky

    请问有人在of中成功使用动态增厚火焰模型吗


  • 重新编译热物理库
    Y yuky

    请问您成功了吗,我也有这方面的需要


  • 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
    Y yuky

    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
    Y yuky

    @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


  • 关于Ansys三维流体域网格导入openfoam的问题
    Y yuky

    同问,我也出现了这个问题,不知道该不该去调整


  • 一个关于 Axisymmetric Subsonic Jet 的问题
    Y yuky

    @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


  • 一个关于 Axisymmetric Subsonic Jet 的问题
    Y yuky

    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


  • 求问ICEM中的楔形网格导入openfoam之后壁面条件如何修改
    Y yuky

    @李东岳 好的,非常感谢东岳老师


  • 求问ICEM中的楔形网格导入openfoam之后壁面条件如何修改
    Y yuky

    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.


  • reactingFoam修改化学反应机理后遇到了问题
    Y yuky

    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:xinlei:
    Create time

    Create mesh for time = 0

    PIMPLE: No convergence criteria found

    PIMPLE: Operating solver in transient mode with 1 outer corrector
    PIMPLE: Operating solver in PISO mode

    Using LTS
    Reading thermophysical properties

    Selecting 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 model

    Selecting combustion model EDC
    Selecting chemistry solver
    {
    solver ode;
    method standard;
    }

    standardChemistryModel: Number of species = 544 and reactions = 2446
    Selecting ODE solver seulex
    Creating field dpdt

    Creating field kinetic energy K

    No MRF models present

    No fvModels present
    No fvConstraints present

    Starting 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-07

    diagonal: 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
    Y yuky

    @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:136: 所以压力出不去


  • openFoam如何调用热物理库中的气体
    Y yuky

    @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


  • reactingFoam报错
    Y yuky

    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:chouchou: 813329af-b8ac-4f33-894a-bc6aec3684c5-12790dce6da29e13d75eb4f1a68eb52.jpg


  • 请问ReactingFoam可否用于气液两相燃烧计算
    Y yuky

    @bestucan 好的好的,十分感谢!


  • reactingFoam修改化学反应机理后遇到了问题
    Y yuky

    @李东岳 好的,谢谢东岳老师,我去看看


  • reactingFoam修改化学反应机理后遇到了问题
    Y yuky

    这个问题解决了,但是出现了新的问题:136:

    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)

  • reactingFoam修改化学反应机理后遇到了问题
    Y yuky

    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

  • reactingFoam计算速度的问题
    Y yuky

    @香柏树 请问你用ReactingFoam ras改les成功了吗,想和您请教一下


  • 用rhoReactingFoam对燃烧瞬态过程进行求解
    Y yuky

    @myheart 好的好的,十分感谢,我再去研究一下


  • 请问ReactingFoam可否用于气液两相燃烧计算
    Y yuky

    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

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