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France-Japan joint Seminar on Thermal fatigue, 5 th to 6 th October 2009, Tokyo, Japan. LES and URANS predictions using Star-CD V&V for T-Junction test case (Vattenfall Experiment) Part of UK’s “ K eeping N uclear O ptions O pen” project. Presented by: Y. Addad
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France-Japan joint Seminar on Thermal fatigue, 5th to 6th October 2009, Tokyo, Japan. LES and URANS predictions using Star-CD V&V for T-Junction test case (Vattenfall Experiment) Part of UK’s “Keeping Nuclear Options Open” project Presented by: Y. Addad Collaborators: A. Keshmiri, S. Rolfo, M. Cotton, D. Laurence School of Mechanical, Aerospace & Civil Engineering (MACE) The University of Manchester
Rod Bundle arranged in a triangular array SFR fuel assembly Re=11,000 Liquid sodium Exp. f=13Hz The person to contact: www.cfd.mace.manchester.ac.uk/Main/StefanoRolfo
Thermal mixing in T-Junction: Previous work:
Experiment of thermal mixing in T-Junction Flow Ratio: Qc/Qh=2 T = 15°C DC=0.14 m, Dh=0.1m ReC=105 , Reh=105 Previous LES runs with Fluent (see reference) Reference: Westin J. et al. “High-Cycle Thermal Fatigue in Mixing Tees. Large-Eddy Simulations Compared to a New Validation Experiment”, 16thInt. Conf. On Nuclear Engineering (ICONE-16).
Thermal mixing in T-Junction: Grid 3.1Dh 3Dc 13Dc Grid Cells= 2.56 M. LES RUNS: SGS Model: Smago. PrSGS=0.9 (Default). URANS RUNS: Non-linear k- model Suga et al. 2006. Numerical schemes: 2nd order in space. 2nd order in time.
Inlet Boundary conditions (cyclic RANS) Hot Cold Hot Cold
Instantaneous Temperature variation LES versus URANS LES run Experiment URANS run
Time-averaged V & Temp. in cross sections Plan 2.6D Plan 6.6D URANS Recirculation LES
Velocity Profiles at the plan x=2.6D z 2.6D x
z 2.6D x Velocity fluctuations Profiles at the plan x=2.6D
Velocity Profiles at the plan x=6.6D z 6.6D x Resolved part only
Z T Y L R B T variation at 1mm from walls along the x axis.
LES LES U URANS URANS W
Z T Y L R B Trms variation at 1 mm from walls along the x axis
Z Y Centre Variation of the velocity fluctuations along the x axis in the centre.
Time history of temperature near the walls Z 2 Y 3 1 4 Probe1 Probe3 Probe2 Probe4
Spectra of temperature near the walls Z 2 Y 3 1 4
Z 2 Y 3 1 4 Spectra of streamwise velocity near the walls.
- URANS model: - Fails to capture the complex features of the flow. - Most information needed for thermal fatigue studies is lost. - Not able to capture high frequency events. - Can this be improved or other approaches tested (example DES) ?? - LES with Unstructured grids and Professional Software: - Second order accuracy seems OK. • Mesh is extremely important, adapted to (1/10) large eddy scale ? => need unstructured mesh • Work in progress: How about tetrahedral and polyhedral cells, different SGS models?? Conclusions and future work • Acknowledgements: • UK research council project “Keeping the Nuclear Option Open” (KNOO)