Studies on separation control CFD validation test case based on a higher order les model

Collection of Technical Papers - 3rd AIAA Flow Control Conference

Volumn 3, Issue , 2006, Pages 1583-1605

  Biswas, Debasish ^a  

^a TOSHIBA CORPORATION   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; FLOW CONTROL; NAVIER STOKES EQUATIONS; REYNOLDS NUMBER;

FLOW PHYSICS; LARGE EDDY SIMULATION (LES); SIMULATION MODELS;

COMPUTATIONAL FLUID DYNAMICS;

EID: 33845268218     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (14)

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3. Seifert, A., Eliahu, S., Greenblatt, D., and Wygnanski, I., "Use Of Piezoelectric Actuators for Airfoil Separation Control," AIAA Journal, Vol.36, No.8, pp1535-1537, 1998.
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9. Biswas, D., et. al., "Calculation of Transitional Boundary Layers with an Improved Low-Reynolds Number Version k-εTurbulence model," ASME Journal of Turbomachinery, vol.116, pp.765-773, 1994.
10. Nagano, Y., and Tagawa, M., "An Improved K-ε Model for Boundary Layer Flows," ASME Journal of Fluid Engineering, Vol.112, pp.33-39, 1990.
11. Fujisawa, N., "Calculations of Transitional Boundary Layer with a Refined Low-Reynolds-Number Version of a K-ε Model of Turbulence," Engineering Turbulence Modeling and Experiments, Elsevier Science Publishing Co.,pp.23-32, 1990.
12. The web site of Langley Research Center Workshop (CFD Validation of Synthetic Jets and Turbulent Separation Control), 2004.
13. Philip E. Morgan, Donald P. Rizzetta, and Miguel R. Visbal, "Large Eddy Simulation of Separation Control for Flow Over a Wall-Mounted Hump," AIAA Paper, AIAA 2005-5017.
14. Seifert, A and Pack, L.G., "Active Flow Separation Control On wall Mounted Hump at High Reynolds Numbers," AIAA Journal, Vol.40, No.7, 2002.