Lecture 10 - Turbulence Models Applied Computational Fluid Dynamics Instructor: Andr Bakker Andr Bakker (2002-2005) Fluent Inc. (2002) 1 Turbulence models A turbulence model is a computational procedure to close the system of mean flow equations. For most engineering applications it is unnecessary to resolve the details of the turbulent fluctuations. Turbulence models allow the calculation of the mean flow without first calculating the full time-dependent flow field. We only need to know how turbulence affected the mean flow. In particular we need expressions for the Reynolds stresses. For a turbulence model to be useful it:
must have wide applicability, be accurate, simple, and economical to run. 2 Common turbulence models Classical models. Based on Reynolds Averaged Navier-Stokes (RANS) equations (time averaged): 1. Zero equation model: mixing length model. 2. One equation model: Spalart-Almaras. 3. Two equation models: k- style models (standard, RNG, realizable), k- model, and ASM. 4. Seven equation model: Reynolds stress model. The number of equations denotes the number of additional PDEs that are being solved.
Large eddy simulation. Based on space-filtered equations. Time dependent calculations are performed. Large eddies are explicitly calculated. For small eddies, their effect on the flow pattern is taken into account with a subgrid model of which many styles are available. 3 Prediction Methods l h = l/ReL3/4 Direct numerical simulation (DNS) Large eddy simulation (LES) Reynolds averaged Navier-Stokes equations (RANS) 4 Boussinesq hypothesis
Many turbulence models are based upon the Boussinesq hypothesis. It was experimentally observed that turbulence decays unless there is shear in isothermal incompressible flows. Turbulence was found to increase as the mean rate of deformation increases. Boussinesq proposed in 1877 that the Reynolds stresses could be linked to the mean rate of deformation. Using the suffix notation where i, j, and k denote the x-, y-, and zdirections respectively, viscous stresses are given by: ui u j ij eij x j xi Similarly, link Reynolds stresses to the mean rate of deformation: U i U j ij ui ' u j ' t
x x j i 5 Turbulent viscosity A new quantity appears: the turbulent viscosity t. U i U j ij ui ' u j ' t x
x j i Its unit is the same as that of the molecular viscosity: Pa.s. It is also called the eddy viscosity. We can also define a kinematic turbulent viscosity: t = t/. Its unit is m2/s. The turbulent viscosity is not homogeneous, i.e. it varies in space. It is, however, assumed to be isotropic. It is the same in all directions. This assumption is valid for many flows, but not for all (e.g. flows with strong separation or swirl). 6 Turbulent Schmidt number The turbulent viscosity is used to close the momentum equations. We can use a similar assumption for the turbulent fluctuation terms that appear in the scalar transport equations. For a scalar property (t) = + (t):
ui ' ' t xi Here t is the turbulent diffusivity. The turbulent diffusivity is calculated from the turbulent viscosity, using a model constant called the turbulent Schmidt number (AKA Prandtl number) t: t t t Experiments have shown that the turbulent Schmidt number is nearly constant with typical values between 0.7 and 1. 7 Flow around a cylinder The flow is stable for Reynolds numbers below ~40. For higher Reynolds numbers the flow is unstable. This animation shows the flow pattern for Re = 1000. 8
Time average streamlines (kg/s) - Re = 1000 9 Effective viscosity (kg/m-s) - Re =1000 10 Predicting the turbulent viscosity The following models can be used to predict the turbulent viscosity: Mixing length model. Spalart-Allmaras model.
Standard k- model. k- RNG model. Realizable k- model. k- model. We will discuss these one by one. 17 Mixing length model On dimensional grounds one can express the kinematic turbulent viscosity as the product of a velocity scale and a length scale: t (m 2 / s ) (m / s ) (m) If we then assume that the velocity scale is proportional to the length scale and the gradients in the velocity (shear rate, which has dimension 1/s): U y we can derive Prandtls (1925) mixing length model:
2 U t m y Algebraic expressions exist for the mixing length for simple 2-D flows, such as pipe and channel flow. 18 Mixing length model discussion Advantages: Easy to implement. Fast calculation times. Good predictions for simple flows where experimental correlations for the mixing length exist. Disadvantages: Completely incapable of describing flows where the turbulent length scale varies: anything with separation or circulation. Only calculates mean flow properties and turbulent shear stress. Use: Sometimes used for simple external aero flows.
Pretty much completely ignored in commercial CFD programs today. Much better models are available. 19 Spalart-Allmaras one-equation model Solves a single conservation equation (PDE) for the turbulent viscosity: This conservation equation contains convective and diffusive transport terms, as well as expressions for the production and dissipation of t. Developed for use in unstructured codes in the aerospace industry. Economical and accurate for: Attached wall-bounded flows. Flows with mild separation and recirculation. Weak for: Massively separated flows. Free shear flows. Decaying turbulence.
Because of its relatively narrow use we will not discuss this model in detail. 20 The k- model The k- model focuses on the mechanisms that affect the turbulent kinetic energy (per unit mass) k. The instantaneous kinetic energy k(t) of a turbulent flow is the sum of mean kinetic energy K and turbulent kinetic energy k: K 12 U 2 V 2 W 2 k 12 u '2 v'2 w'2 k (t ) K k is the dissipation rate of k. If k and are known, we can model the turbulent viscosity as: k 3/ 2
k2 t k We now need equations for k and . 1/ 2 21 Turbulent kinetic energy k The equation for the turbulent kinetic energy k is as follows: k div( kU) div p' u' 2 u' eij ' 12 ui '.ui ' u j ' 2 eij '.eij ' ( ui ' u j '.Eij ) t II (I ) ( III ) ( IV ) (V ) (VI ) (VII )
Here eij is fluctuating component of rate of deformation tensor. This equation can be read as: (I) the rate of change of k, plus (II) transport of k by convection, equals (III) transport of k by pressure, plus (IV) transport of k by viscous stresses, plus (V) transport of k by Reynolds stresses, minus (VI) rate of dissipation of k, plus (VII) turbulence production. 23 Model equation for k
The equation for k contains additional turbulent fluctuation terms, that are unknown. Again using the Boussinesq assumption, these fluctuation terms can be linked to the mean flow. The following (simplified) model equation for k is commonly used. ( k ) div( kU) div t grad k 2 t Eij .Eij t k Rate of increase Convective transport Diffusive transport Rate of
production Rate of destruction The Prandtl number k connects the diffusivity of k to the eddy viscosity. Typically a value of 1.0 is used. 24 Dissipation rate - analytical equation The analytical equation for is shown below. Because of the many unknown higher order terms, this equation can not be solved, and simplified model equations need to be derived. 26 Model equation for A model equation for is derived by multiplying the k equation by (/k) and introducing model constants. The following (simplified) model equation for is commonly used. t
( ) 2 div( U) div grad C1 2 t Eij .Eij C2 t k k Rate of increase Convective transport Diffusive transport Rate of production
Rate of destruction The Prandtl number connects the diffusivity of to the eddy viscosity. Typically a value of 1.30 is used. Typically values for the model constants C1 and C2 of 1.44 and 1.92 are used. 27 Calculating the Reynolds stresses from k and The turbulent viscosity is calculated from: k2 t C C 0.09 The Reynolds stresses are then calculated as follows: U i U j 2 2
ui ' u j ' t k ij 2 t Eij k ij xi 3 3 x j ij 1 if i j and ij 0 if i j The (2/3)kkij term ensures that the normal stresses sum to k. Note that the k- model leads to all normal stresses being equal, which is usually inaccurate. 28 k- model discussion Advantages: Relatively simple to implement. Leads to stable calculations that converge relatively easily. Reasonable predictions for many flows.
Disadvantages: Poor predictions for: swirling and rotating flows, flows with strong separation, axisymmetric jets, certain unconfined flows, and fully developed flows in non-circular ducts. Valid only for fully turbulent flows. Simplistic equation. 29 More two-equation models The k- model was developed in the early 1970s. Its strengths as
well as its shortcomings are well documented. Many attempts have been made to develop two-equation models that improve on the standard k- model. We will discuss some here: k- RNG model. k- realizable model. k- model. Algebraic stress model. Non-linear models. 30 Improvement: RNG k- k- equations are derived from the application of a rigorous statistical technique (Renormalization Group Method) to the
instantaneous Navier-Stokes equations. Similar in form to the standard k- equations but includes: Additional term in equation for interaction between turbulence dissipation and mean shear. The effect of swirl on turbulence. Analytical formula for turbulent Prandtl number. Differential formula for effective viscosity. Improved predictions for: High streamline curvature and strain rate. Transitional flows. Wall heat and mass transfer. But still does not predict the spreading of a round jet correctly. 31 Improvement: realizable k- Shares the same turbulent kinetic energy equation as the standard k- model. Improved equation for . Variable C instead of constant.
Improved performance for flows involving: Planar and round jets (predicts round jet spreading correctly). Boundary layers under strong adverse pressure gradients or separation. Rotation, recirculation. Strong streamline curvature. 33 k- model This is another two equation model. In this model is an inverse time scale that is associated with the turbulence. This model solves two additional PDEs: A modified version of the k equation used in the k- model. A transport equation for . The turbulent viscosity is then calculated as follows: k Its numerical behavior is similar to that of the k- models. It suffers from some of the same drawbacks, such as the
assumption that t is isotropic. t 37 Algebraic stress model The same k and equations are solved as with the standard k- model. However, the Boussinesq assumption is not used. The full Reynolds stress equations are first derived, and then some simplifying assumptions are made that allow the derivation of algebraic equations for the Reynolds stresses. Thus fewer PDEs have to be solved than with the full RSM and it is much easier to implement. The algebraic equations themselves are not very stable, however, and computer time is significantly more than with the standard k- model. This model was used in the 1980s and early 1990s. Research continues but this model is rarely used in industry anymore now that most commercial CFD codes have full RSM implementations
available. 38 Non-linear models The standard k- model is extended by including second and sometimes third order terms in the equation for the Reynolds stresses. One example is the Speziale model: 3 2 k2 k ij ui ' u j ' k ij C 2 Eij 4C D C 2 2 * f ( E , E / t , u, U / x) 3 Here f() is a complex function of the deformation tensor, velocity field and gradients, and the rate of change of the deformation tensor. The standard k- model reduces to a special case of this model
for flows with low rates of deformation. These models are relatively new and not yet used very widely. 39 Reynolds stress model RSM closes the Reynolds-Averaged Navier-Stokes equations by solving additional transport equations for the six independent Reynolds stresses. Transport equations derived by Reynolds averaging the product of the momentum equations with a fluctuating property. Closure also requires one equation for turbulent dissipation. Isotropic eddy viscosity assumption is avoided. Resulting equations contain terms that need to be modeled. RSM is good for accurately predicting complex flows. Accounts for streamline curvature, swirl, rotation and high strain rates. Cyclone flows, swirling combustor flows. Rotating flow passages, secondary flows. Flows involving separation. 40
Reynolds stress transport equation The exact equation for the transport of the Reynolds stress Rij: DRij Pij Dij ij ij ij Dt This equation can be read as: rate of change of Rij ui ' u j ' plus transport of Rij by convection, equals rate of production Pij, plus transport by diffusion Dij, minus rate of dissipation ij, plus transport due to turbulent pressure-strain interactions ij, plus transport due to rotation ij. This equation describes six partial differential equations, one for the transport of each of the six independent Reynolds stresses. 41 Reynolds stress transport equation The various terms are modeled as follows:
Production Pij is retained in its exact form. Diffusive transport Dij is modeled using a gradient diffusion assumption. The dissipation ij, is related to as calculated from the standard equation, although more advanced models are available also. Pressure strain interactions , are very important. These include ij pressure fluctuations due to eddies interacting with each other, and due to interactions between eddies and regions of the flow with a different mean velocity. The overall effect is to make the normal stresses more isotropic and to decrease shear stresses. It does not change the total turbulent kinetic energy. This is a difficult to model term, and various models are available. Common is the Launder model. Improved, non-equilibrium models are available also. Transport due to rotation ij is retained in its exact form. 42 Setting boundary conditions Characterize turbulence at inlets and outlets (potential backflow). k- models require k and . Reynolds stress model requires Rij and .
Other options: Turbulence intensity and length scale. Length scale is related to size of large eddies that contain most of energy. For boundary layer flows, 0.4 times boundary layer thickness: l 0.499. For flows downstream of grids /perforated plates: l opening size. Turbulence intensity and hydraulic diameter. Ideally suited for duct and pipe flows. Turbulence intensity and turbulent viscosity ratio. For external flows: 1 / t 10 45
Comparison of RANS turbulence models Model SpalartAllmaras STD k- RNG k- Realizable k- Reynolds Stress Model Strengths Weaknesses Economical (1-eq.); good track record for mildly complex B.L. type of flows. Robust, economical, reasonably accurate; long accumulated performance
data. Not very widely tested yet; lack of submodels (e.g. combustion, buoyancy). Good for moderately complex behavior like jet impingement, separating flows, swirling flows, and secondary flows. Offers largely the same benefits as RNG but also resolves the round-jet anomaly. Mediocre results for complex flows with severe pressure gradients, strong streamline curvature, swirl and rotation. Predicts that round jets spread 15% faster than planar jets whereas in actuality they spread 15% slower. Subjected to limitations due to isotropic eddy viscosity assumption. Same problem with
round jets as standard k-. Subjected to limitations due to isotropic eddy viscosity assumption. Physically most complete Requires more cpu effort (2-3x); tightly model (history, transport, and coupled momentum and turbulence anisotropy of turbulent equations. stresses are all accounted for). 46 Recommendation Start calculations by performing 100 iterations or so with standard k- model and first order upwind differencing. For very simple flows (no swirl or separation) converge with second order upwind and k- model. If the flow involves jets, separation, or moderate swirl, converge solution with the realizable k- model and second order differencing. If the flow is dominated by swirl (e.g. a cyclone or unbaffled stirred
vessel) converge solution deeply using RSM and a second order differencing scheme. If the solution will not converge, use first order differencing instead. Ignore the existence of mixing length models and the algebraic stress model. Only use the other models if you know from other sources that somehow these are especially suitable for your particular problem (e.g. Spalart-Allmaras for certain external flows, k- RNG for certain transitional flows, or k-). 47
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