UFR 1-06 Evaluation

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Axisymmetric buoyant far-field plume in a quiescent unstratified environment

Underlying Flow Regime 1-06

Comparison of CFD Calculations with Experiments

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Van Maele & Merci [2] presented the results from a number of simulations that examined the effects of different combinations of models and approximations. The Boussinesq approximation $({\overline {\rho }}\approx \rho _{\infty })$ was shown to have no affect on the model predictions when the SGDH model was used. Indeed, the SGDH source term itself had a negligible influence on the results. When using the GGDH source term, however, the Boussinesq approximation had an effect on the results nearest to the plume exit at z/D = 12, where the assumption of $({\overline {\rho }}\approx \rho _{\infty })$ caused an increase in the peak velocity of around 5%. By assuming that the mean density was the same as the reference density, the buoyancy source term became smaller and so the turbulent kinetic energy and hence the eddy viscosity were also smaller. As a consequence, there was less mixing, the centreline velocity increased and the spreading rate decreased. The effect was significant where the mean density differed most from the reference density, nearest to the plume source, but was negligible in the far field. These results suggest that the Boussinesq approximation can be used in the far field of buoyant plumes where density differences are small. However, if the CFD domain extends from the far field to the source of buoyancy, such as a fire or strongly heated surface where density differences are appreciable, then the Boussinesq approximation should not be used.

It should also be remembered that Van Maele & Merci’s interpretation of the ‘Boussineq approximation’ only involved setting $({\overline {\rho }}\approx \rho _{\infty })$ in the production term, G. The density and other flow properties (molecular viscosity, specific heat etc.) still varied as a function of temperature elsewhere in the transport equations.

Van Maele & Merci examined the effects of SGDH versus GGDH and the effect of switching on and off both the production due to buoyancy term, G, and the source term in the ε–equation, S_εB, on the standard and realizable k – ε models. Table 4 summarizes the cases tested. In the relevant cases, they used the full buoyancy source term G rather than any truncated form of the equation. The ε–equations were different for standard and realizable models, but in both cases, where used, the buoyancy-related source term was given by:

$\ \ \ \ \ \ \ \ S_{\varepsilon B}=c_{\varepsilon 1}\left(1-c_{\varepsilon 3}\right){\frac {\varepsilon }{k}}G\ \qquad {\text{with}}\ \ c_{\varepsilon 3}=0.8$

$\left(35\right)$

The results were compared to the experimental data of George&'et al. [3] and the correlations of Shabbir & George [11] which were given by:

Axial velocity:

$WF_{0}^{-1/3}z^{1/3}=3.4\exp \left(-58\eta ^{2}\right)$

$\left(36\right)$

Buoyancy:

$g\beta \Delta TF_{0}^{-2/3}z^{5/3}=9.4\exp \left(-68\eta ^{2}\right)$

$\left(37\right)$

where W is the mean axial momentum, ΔT is the difference between the local mean and ambient temperatures, z is the vertical distance from the source, η = r/z is the similarity variable (r is the radial distance from the plume centreline), and β the thermal expansion coefficient. The buoyancy added at the source, F₀ , is found from :

$F_{0}=2\pi \int _{0}^{r_{0}}Wg{\frac {\delta \rho }{\rho _{\infty }}}r{\text{d}}r$

$\left(38\right)$

and was 1.0 × 10^-6 cm⁴/s³ in the George et al. plume [3]. To compare to these empirical correlations, Van Maele & Merci used their results taken at a position, z = 1.75 m, equivalent to approximately 28 inlet diameters from the source. To demonstrate that this was sufficiently far from the source to produce self-similar profiles, the dimensionless velocity and temperature profiles were shown to be practically identical at a distance of 2.75 m.

Profiles of the mean axial velocity and buoyancy are compared to the empirical correlations in Figures 7 and 8. A summary of the centreline values and spreading rates for velocity and temperature are given in Table 5. This shows the measured values from the experiments of George et al. [3], the recommended values given by Chen & Rodi [1] from their analysis of plume experiments up to 1980, the subsequent measured values from Shabbir & George [11], the RANS results from Van Maele & Merci [2] and Hossain & Rodi, and the LES results from Zhou et al. [28]. Three results are taken from Hossain & Rodi: Case A which is from a k – ε model without any buoyancy modifications, Case B which is from a k – ε model with buoyancy corrections in both k and ε equations, and Case C which is from Hossain & Rodi’s algebraic stress/flux model.

For the Van Maele & Merci [2] results, both the standard and realizable k – ε models without buoyancy modifications (cases SKE and RKE) predicted overly large centreline velocity and buoyancy values and under-predicted the spreading rates of the plume. When the SGDH source term was used, with or without S_εB , it had practically no effect on the results. This may have been partly due to the particular choice of the constant c_ε3 which made the contribution from the buoyancy production small relatively to shear production in the ε-equation. The SKE, SKE_A and SKE_A* cases all returned very similar predictions to each other and RKE, RKE_A and RKE_A* cases behaved similarly. This was shown by Van Maele & Merci to be a consequence of the SGDH source term being negligible in comparison to other terms in the k and ε equations.

Table 5 shows that for the basic k – ε model without any buoyancy corrections there are significant differences in terms of the predicted spreading rates between the results of Van Maele & Merci [2] and Hossain & Rodi [8] (cases SKE and A, respectively). Van Maele & Merci’s predictions of the spreading rates are nearly 20% higher. This may have been due to the choice of non-standard model constants by Hossain & Rodi [8] who used c_μ = 0.109 and σ_t = 0.614, whilst Van Maele & Merci [2] used c_μ = 0.09 and σ_t = 0.85. The results for the k – ε model with buoyancy corrections are more similar (Cases SKE_A and B, respectively). Here, in addition to the non-standard c_μ and σ_t constants, Hossain & Rodi [8] used a model with constant c_ε3 scaled by the Richardson number, which was zero in the vertical buoyant plume, such that the buoyancy production had the same weight as the shear production.

Use of the GGDH model produced some improvements in the results presented by Van Maele & Merci [2]. For the SKE_B model, the centreline value was well-predicted but the half-width of the plume was overpredicted by around 20%. When the buoyancy source term in the ε-equation was omitted (case SKE_B*) the axial velocity on the centreline was reduced and the half-width prediction became even more inaccurate. This is consistent in the SKE_B* case with the turbulent kinetic energy being overpredicted due to the removal of a positive source in the ε-equation.

For the realizable model with GGDH, the mean axial velocity and buoyancy were over-predicted on the centreline by around 10% and 20% respectively but the half-width was reasonably close to the experimental values. Switching off the buoyancy-related source term in the ε-equation (case RKE_B*) led to a slight improvement in the results, however Van Maele & Merci noted that this also reduced the numerical stability of the calculation. Details of any source-term linearisation used to improve robustness are not provided in their paper. They recommended that the S_εB term should be retained in the modelled equations to avoid convergence difficulties.

Van Maele & Merci commented that, overall, the GGDH variant of the realizable model (RKE_B) performed better than the equivalent standard k – ε model (SKE_B). However, the standard model gave better peak mean axial velocity and buoyancy predictions (to within 2% and 10%, respectively, compared to 10% and 25% for the RKE_B model). It could also be argued that the realizable model only gives good predictions for the plume half-width because the predicted profiles happen to cross the experiment profiles at the correct position, the actual shape of the predicted profiles are incorrect. One could conclude, perhaps, that both standard and realizable models predict the axisymmetric plume to a similar overall level of accuracy. Neither provides an exact solution and the errors for the two models are slightly different.

Table 4 Summary of the model variants tested by Van Maele & Merci [2]

Case Ref.	Turbulence Model	G	SεB
SKE	Standard k – ε	–	–
SKE_A	Standard k – ε	SGDH	Eqn (35)
SKE_A*	Standard k – ε	SGDH	–
SKE_B	Standard k – ε	GGDH	Eqn (35)
SKE_B*	Standard k – ε	GGDH	–
RKE	Realizable k – ε	–	–
RKE_A	Realizable k – ε	SGDH	Eqn (35)
RKE_A*	Realizable k – ε	SGDH	–
RKE_B	Realizable k – ε	GGDH	Eqn (35)
RKE_B*	Realizable k – ε	GGDH	–

Figure 7 Mean axial velocity profiles expressed in terms of similarity variables, from Van Meale & Merci [2]

Figure 8 Mean buoyancy profiles expressed in terms of similarity variables, from Van Meale & Merci [2]

Table 5 Centreline values and half-widths of the plume in terms of mean axial velocity and buoyancy

	(WF0-1/3z1/3)c	lW/2	(gβΛTF0-2/3z5/3)c	lΔT/2
George et al. [3] experiments	3.4	0.112	9.1	0.104
Chen & Rodi [1] recommendation	3.5	0.112	9.35	0.10
Shabbir & George [11] experiments	3.4	0.107	9.4	0.10
SKE	4.08	0.097	12.76	0.089
SKE_A	4.04	0.098	12.59	0.089
SKE_A*	4.04	0.098	12.55	0.089
SKE_B	3.32	0.132	8.48	0.119
SKE_B*	3.09	0.147	7.35	0.132
RKE	4.35	0.084	15.55	0.079
RKE_A	4.31	0.085	15.36	0.080
RKE_A*	4.3	0.085	15.31	0.080
RKE_B	3.74	0.103	11.78	0.098
RKE_B*	3.62	0.108	11.09	0.103
Hossain & Rodi [8] CFD A	—	0.079	—	0.076
Hossain & Rodi [8] CFD B	—	0.100	—	0.095
Hossain & Rodi [8] CFD C	3.50	0.109	8.22	0.100
Zhou et al LES [28]	—	0.111	—	0.105

Van Maele & Merci also presented results for the streamwise and radial normal Reynolds stresses, ${\overline {\mathit {ww}}}$ and ${\overline {\mathit {uu}}}$ (not shown here). None of the models tested were capable of resolving the anisotropy in the normal stresses, although this is not unexpected since eddy-viscosity models like those tested by Van Maele & Merci were not designed to determine individual normal Reynolds stresses, only their sum, the turbulent kinetic energy. In the experiments, the streamwise stress was greater than the radial stress on the centreline, ${\overline {\mathit {ww}}}\approx 1.6{\overline {\mathit {uu}}}$. The linear k – ε models on the other hand all gave ${\overline {\mathit {ww}}}\approx {\overline {\mathit {uu}}}$. Shear stresses were also not predicted very well and models overpredicted the peak value by up to 25%.

Plots of the k-profiles for standard and realizable models are shown in Figure 9. When normalized using similarity variables all of the models produced an off-axis peak in k which was not present in the experiments. Similar behaviour was observed in plane plumes by Yan & Holmstedt [53]. All standard k – ε model variants underpredicted the centreline turbulent kinetic energy by around 15% whereas the realizable models were all in good agreement with the experiments. However, none of the model variants captured the correct shape of the k-profile.

Figure 9 Profiles of turbulent kinetic energy, made dimensionless using similarity variables, from Van Meale & Merci [2]

Comparison to Other Model Predictions

To provide some comparison to other models’ performance in this flow, the results of Yan & Holmstedt [53] are shown in Figure 10 for the George et al. [3] axisymmetric plume. The “standard model” they refer to is a standard k – ε model with SGDH, whilst “this model” is a modified k – ε model with GGDH that uses an algebraic relation for the Reynolds stresses where they appear in the production term, P_k. The standard model results are in good agreement with those obtained by Van Maele & Merci for the same case. The results obtained using their modified model appear to be better than those obtained by Van Maele & Merci for the standard k – ε model with GGDH.

Figure 10 Normalized mean velocity and buoyancy profiles from Yan & Holmstedt [53]

The predictions of mean velocity and temperature from Hossain & Rodi [8] using an Algebraic Stress Model (ASM) are shown in Figure 11. As noted in Section 2.3.1, their model was derived from the differential stress model of Gibson & Launder [46]. Figure 11 shows that their predictions are in good agreement with the measurements of George et al. [3]. The predicted plume centreline values and half-widths using their model are shown in Table 5 (marked “Hossain & Rodi [8] CFD C”). These exhibit the best agreement with the measurements of George et al. [3] of all the model variants tested.

Figure 11 Normalized mean velocity and temperature profiles from Hossain & Rodi [8]

LES predictions from Zhou et al. [28] of the mean velocity and temperature for the experiments of George et al. [3] are shown in Figure 12. Very good agreement is obtained although this may be partly a consequence of using centreline values to make the mean parameters dimensionless. Radial profiles of normalized RMS axial velocity and temperature were reported to produce a similar trend to that observed in the experiments, and turbulence levels within the experimental range  [29], although the centreline dimensionless temperature fluctuation was approximately 0.45, in good agreement with the measurements of Papanicolaou & List [9] and Dai et al. [10], but slightly higher than the value of 0.40 reported by George et al. [28]. Plume spreading rates and centreline values were found to be strongly sensitive to the imposed turbulent fluctuations at the inlet plane in the LES model. Axial velocity fluctuations with an amplitude of 20% of the mean axial velocity were imposed at the inlet, with or without azimuthal forcing, to match the predicted location of the transition from laminar to turbulent flow to that observed in the experiments. In the experiments, however, the turbulence intensity at the inlet was reported to be approximately 0.5% [11].

Figure 12 Radial profiles of (a) mean axial velocity and (b) mean temperature

at four axial positions compared to the experiments of George et al. [3], from the LES of

Zhou et al. [28].

Figure 13 shows the dimensionless mean axial velocity profiles from Brescianini & Delichatsios [42]. Both the experimental results of George et al. [3] and Dai et al. [39] are shown. The basic model “ke1 Model A” is a standard k – ε model with SGDH. Other model results shown include “keS Model B”: a parabolic k – ε model based on the work of Hanjalić & Launder [76] which retains both shear and normal-stress production terms, together with GGDH for the production term due to buoyancy; “keS Model C1”: the same k – ε model but with the streamwise turbulent scalar flux determined using the algebraic model of Hossain & Rodi [8] and “keS Model C2”: an extension of the C1 model that retains streamwise gradients of velocity and density. The three “keS” model variants all produce similar results that are in good agreement with the experiments of George et al. [3]. Interestingly, the standard k – ε model with SGDH produces results in good agreement with the experimental data of Dai et al. [39] but in poor agreement with the data of George et al. [3] Brescianini & Delichatsios [42] commented that the results of their assessment depend strongly upon which set of experiments are used for comparison.

Figure 13 Mean axial velocity profiles from

Brescianini & Delichatsios [42]. The quantity U on the y-axis is dimensionless and equivalent to (WF₀^-1/3z^1/3)

in Van Maele & Merci's notation.

Summary

Van Maele & Merci’s [2] results for two different linear k – ε models have been presented for the axisymmetric buoyant plume of George et al. [3] Various modifications to the buoyancy treatment and other simplifications were tested. From this work, the following conclusions can be drawn:

• The Boussinesq approximation can be used to model the flow behaviour in far-field of buoyant plumes, where density differences are small. Nearer the source of buoyancy, where density differences are more appreciable, the approximation should be used with care. In Van Maele & Merci’s [2] study it was shown to have no effect if SGDH is used, but had a noticeable effect with GGDH.
• The SGDH buoyancy-production term, G, is calculated using the streamwise temperature gradient which is small in this flow and the term therefore has little effect on the mean flow behaviour. As a consequence, when using SGDH the turbulent kinetic energy is underpredicted, the plumes have overly large centreline velocity and temperature values and do not spread sufficiently quickly.
• Using GGDH instead of SGDH improves the mean flow predictions.
• Neglecting the buoyancy source term, S_εB, in the ε-equation has a relatively minor effect on the results with GGDH but can cause numerical stability problems. It is therefore not recommended to neglect this term.
• Van Maele & Merci assert that the realizable k – ε model of Shih et al. [66] when combined with GGDH performs better than the standard k – ε model with GGDH. However, the overall improvement shown in their results is relatively modest, if present at all.
• Better predictions of the mean flow behaviour in the far-field of buoyant plumes have been obtained using the more sophisticated k – ε model of Yan & Holmstedt [52] and the ASM of Hossain & Rodi [8].

Front Page

Description

Test Case Studies

Evaluation

Best Practice Advice

References

Contributed by: Simon Gant — Lea Associates

© copyright ERCOFTAC 2010