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RAS and DES transition models for OpenFOAM-v2012

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transition-models

RAS transition models

kOmegaSSTGam

Description

A One-Equation Local Correlation-Based Transition Model based on the k-omega-SST RAS model.

References

Menter, F.R., Smirnov, P.E., Liu, T. et al. (2015). A One-Equation Local Correlation-Based Transition Model. Flow Turbulence Combust 95, 583–619.

kOmegaSSTLMK1

Description

Langtry-Menter 4-equation transitional SST model based on the k-omega-SST RAS model with Krause's correlations.

References

Langtry, R. B., & Menter, F. R. (2009). Correlation-based transition modeling for unstructured parallelized computational fluid dynamics codes. AIAA journal, 47(12), 2894-2906.
Menter, F. R., Langtry, R., & Volker, S. (2006). Transition modelling for general purpose CFD codes. Flow, turbulence and combustion, 77(1-4), 277-303.
Langtry, R. B. (2006). A correlation-based transition model using local variables for unstructured parallelized CFD codes. Phd. Thesis, Universität Stuttgart.
Krause M, Behr M, Ballmann J. (2008). Modeling of Transition Effects in Hypersonic Intake Flows Using a Correlation-Based Intermittency Model. 15th AIAA International Space Planes and Hypersonic
Systems and Technologies Conference.

kOmegaSSTLMK2

Description

Langtry-Menter 4-equation transitional SST model based on the k-omega-SST RAS model with Krause's correlations for hypersonic flow.

References

Langtry, R. B., & Menter, F. R. (2009). Correlation-based transition modeling for unstructured parallelized computational fluid dynamics codes. AIAA journal, 47(12), 2894-2906.
Menter, F. R., Langtry, R., & Volker, S. (2006). Transition modelling for general purpose CFD codes. Flow, turbulence and combustion, 77(1-4), 277-303.
Langtry, R. B. (2006). A correlation-based transition model using local variables for unstructured parallelized CFD codes. Phd. Thesis, Universität Stuttgart.
Frauholz S, Reinartz B U, Müller S, et al. (2014). Transition Prediction for Scramjets Using γ-Reθt Model Coupled to Two Turbulence Models. Journal of Propulsion & Power, 1-19.
Krause M. (2010). Numerical analysis of transition effects for scramjet intake flows. Phd. Thesis, RWTH Aachen University.

kOmegaSSTLMK2Y

Description

Langtry-Menter 4-equation transitional SST model based on the k-omega-SST RAS model combined Krause's correlations for hypersonic flows with You's modifications for separated transitional flows.

References

Langtry, R. B., & Menter, F. R. (2009). Correlation-based transition modeling for unstructured parallelized computational fluid dynamics codes. AIAA journal, 47(12), 2894-2906.
Menter, F. R., Langtry, R., & Volker, S. (2006). Transition modelling for general purpose CFD codes. Flow, turbulence and combustion, 77(1-4), 277-303.
Langtry, R. B. (2006). A correlation-based transition model using local variables for unstructured parallelized CFD codes. Phd. Thesis, Universität Stuttgart.
Frauholz S, Reinartz B U, Müller S, et al. (2014). Transition Prediction for Scramjets Using γ-Reθt Model Coupled to Two Turbulence Models. Journal of Propulsion & Power, 1-19.
Krause M. (2010). Numerical analysis of transition effects for scramjet intake flows. Phd. Thesis, RWTH Aachen University.
You Y, Luedeke H, Eggers T, et al. (2013). Application of the γ-Reθt Transition Model in High Speed Flows. Aiaa/3af International Space Planes & Hypersonic Systems & Technologies Conference. 

DES transition models

kOmegaSSTDES

Description

k-omega-SST DES turbulence model modified according to Menter & Kuntz (2004).

Usage

FSST  0;
//- Zonal filter choice
//
// - 0: no filtering
// - 1: (1 - F1)
// - 2: (1 - F2)

References

Strelets, M. (2001). Detached Eddy Simulation of Massively Separated Flows, 39th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV
Menter, F.R., Kuntz, M. (2004). Adaptation of Eddy-Viscosity Turbulence	Models to Unsteady Separated Flow Behind Vehicles. In: McCallen, R., Browand, F., Ross, J. (eds) The Aerodynamics of Heavy Vehicles: Trucks, Buses, and Trains. Lecture Notes in Applied and Computational Mechanics, vol 19. Springer, Berlin, Heidelberg.

kOmegaSSTGamDES

Description

A One-Equation Local Correlation-Based Transition Model based on the k-omega-SST DES model.

References

Menter, F.R., Smirnov, P.E., Liu, T. et al. (2015). A One-Equation Local Correlation-Based Transition Model. Flow Turbulence Combust 95, 583–619.

kOmegaSSTLMDES

Description

Langtry-Menter 4-equation transitional SST model based on the k-omega-SST DES model.

References

Langtry, R. B., & Menter, F. R. (2009). Correlation-based transition modeling for unstructured parallelized computational fluid dynamics codes. AIAA journal, 47(12), 2894-2906.
Menter, F. R., Langtry, R., & Volker, S. (2006). Transition modelling for general purpose CFD codes. Flow, turbulence and combustion, 77(1-4), 277-303.
Langtry, R. B. (2006). A correlation-based transition model using local variables for unstructured parallelized CFD codes. Phd. Thesis, Universität Stuttgart.
Nakhostin, S.M. (2019). Investigation of transitional turbulence models to predict drag crisis for flow over spheres and cylinder. Master's Thesis, Universitetet i Stavanger.

tutorials

Description

ERCOFTAC T3A 3% test-case

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RAS and DES transition models for OpenFOAM-v2012


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