A pressure gradient sensitive wall function for the prediction of turbulent flow in thermal turbomachinery

Proceedings of the ASME Turbo Expo

Volumn 6 PART B, Issue , 2005, Pages 1089-1098

  Pieringer, Paul ^a   Sanz, Wolfgang ^a  

^a GRAZ UNIVERSITY OF TECHNOLOGY   (Austria)

Author keywords

[No Author keywords available]

Indexed keywords

ECONOMICAL DESIGN; PRESSURE GRADIENT; SECONDARY FLOW;

BOUNDARY LAYERS; COMPUTATIONAL FLUID DYNAMICS; PRESSURE EFFECTS; STRESS CONCENTRATION; TURBOMACHINERY; TURBULENT FLOW;

GAS TURBINES;

EID: 27744502825     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/GT2005-68471     Document Type: Conference Paper

References (8)

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3. Kim, S.-E., and Choudhury, D., 1995. "A near-wall treatment using wall functions sesitized to pressure gradient". ASME FED, Separated and Complex Flows, 217.
4. Spalart, P., and Allmaras, S., 1992. "A one-equation turbulence model for aerodynamic flows". AIAA Paper 92-0439.
5. Erhare, J., and Gehrer, A., 2000. "Design and construction of a transonic test-turbine facility". ASME (2000-GT-480).
6. Goettlich, E., Neumayer, F., Woisetschlaeger, J., Sanz, W., and Heitmeier, F., 2004. "Investigation of stator rotor interaction in a transonic turbine stage using laser doppler velocimetry and pneumatic probes". ASME Journal of Turbomachinery, 126, pp. 297-305.
7. th European Conference on Turbomachinery, pp. 1061-1075.
8. th European Conference on Turbomachinery.