On the calculation of Reynolds stresses by CFD

35th AIAA Fluid Dynamics Conference and Exhibit

Volumn , Issue , 2005, Pages

  Guo, Yueping ^a   Chang, Kuo Cheng ^a  

^a BOEING COMPANY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ANISOTROPIC STRESS; EXPLICIT ALGEBRAIC STRESS MODEL; FEASIBILITY STUDIES; NOISE GENERATION MECHANISMS; NORMAL AND SHEAR STRESS; QUANTITATIVE COMPARISON; TURBULENCE KINETIC ENERGY; TURBULENCE PARAMETERS;

ANISOTROPY; COMPUTER SIMULATION; DATA PROCESSING; KINETICS; REYNOLDS NUMBER; TOOLS; TURBULENCE MODELS; TURBULENT FLOW;

COMPUTATIONAL FLUID DYNAMICS;

EID: 84884935503     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (24)

1. Abid, R. "Evaluation of two-equation turbulence models for predicting transitional flows" International Journal of Engineering Science, 31, 831-840, 1993.
2. Abid R., Rumsey C. and Gatski T. B. 1995 Prediction of nonequilibrium turbulent flows with explicit algebraic stress models. AIAA Journal, 33(11), 2026-2031.
3. Abid R., Morrison J. H., Gatski T. B. and Speziale C. G. 1996 Prediction of complex aerodynamic flows with explicit algebraic stress models. AIAA Paper 96-0565.
4. Bradshaw P., Ferries D. H. and Atwell N. P. 1967 Calculation of boundary layer development using the turbulent energy equation. J. Fluid Mech. 28(3), 593-616.
5. Gatski T. B. 1996 Prediction of airfoil characteristics with higher order turbulence models. NASA TM 110246.
6. Goldstein M. E. 1976 Aeroacoustics. McGraw-Hill.
7. Hedges L. S. 2000 A tool to convert SA and SST turbulenct transport quantities in to k-turbulent transport quantities. Boeing Internal Memo, ER&D-BBAN5-2000-007.
8. Lilley, M. G. 1994 The Radiated Noise from Isotropic Turbulence Revisited, Theoret. & Comput. Fluid Dyn, 6 281-301.
9. Lighthill M. J. 1952 On sound generated aerodynamically: I. General theory. Roc. Roy. Soc. Lond. A211, 564-587.
10. Menter F. R 1993 Z onal two equation k-+ turbulence models for aerodynamic flows. AIAA 93-2906.
11. Nakayama A. 1982 Measurements in the boundary layer and wake of two airfoil models. MDC Report No. J2403.
12. Nakayama A. 1985 Characteristics of the flow around conventional and supercritical airfoils. J. Fluid Mech. 160, 155-179.
13. Patel V. C., Rodi W. and Scheuerer G. 1985 Turbulence Models for nearwall and low Reynolds number flows: a review. AIAA J. 23, 1308-1319.
14. Patel V. C. and Sheuerer G. 1982 Calculation of tow-dimensional near and far wakes. AIAA J. 20(7), 900-907.
15. Pot P. J. 1979 Measurements in a 2-D wake and in a 2-D wake merging into a boundary layer. NLR TR 79063U.
16. Ramaprian B. R., Patel V. C. and Sastry M. S. 1981 Turbulent wake development behind streamlined bodies. Iowa Institute of Hydraulic Research, Iowa City, IIHR Report. 231.
17. Rumsey C. L. and Gatski T. B. 2000 Recent turbulence model advances applied to multi-element airfoil computations. AIAA 2000-4323.
18. Shih T. H., Zhu J. & Lumley J. L. 1994 A new Reynolds stress algebraic equation model. NASA TM 106644.
19. Spalart P. R. 2000 How to turn a good model into k. Private research notes, dated March 2000.
20. Spalart P. R. and Allmaras S. R. 1992 A one-equation turbulence model for aerodynamic flow. AIAA Paper 92-439, Reno, NV.
21. Tannehill J. C., Anderson D. A. and Pletcher R. H. 1997 Computational Fluid Mechanics and Heat Transfer. Taylor & Francis Publishers. Washington DC.
22. nd ed., Cambridge University Press, New York.
23. Wilcox D. C. 1993 Turbulence Modeling for CFD. DCW Industries, Inc. California.
24. Xu X. H. and Speziale C. G. 1996 Explicit algebraic stress model for turbulence with anisotropic dissipation. AIAA Journal, 34(10), 2186-2189.