Scaling of the turbulent boundary layer along a flat plate according to different turbulence models

International Journal of Heat and Fluid Flow

Volumn 19, Issue 4, 1998, Pages 338-347

  Henkes, R A W M ^a,b  

^a SRTCA   (Netherlands)

^b DELFT UNIVERSITY OF TECHNOLOGY   (Netherlands)

Author keywords

[No Author keywords available]

Indexed keywords

ALGEBRA; COMPUTER SIMULATION; KINETIC ENERGY; PROBLEM SOLVING; REYNOLDS NUMBER; SHEAR STRESS; TURBULENCE; VELOCITY; VISCOSITY;

DEFECT LAW; TURBULENT BOUNDARY LAYER;

BOUNDARY LAYERS;

BOUNDARY LAYER; SCALING; TURBULENT FLOW;

BOUNDARY LAYER; FLOW MODELING; TURBULENT FLOW;

EID: 0032144572     PISSN: 0142727X     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0142-727X(98)10009-7     Document Type: Article

References (23)

1. Barenblatt, G.I., 1993. Scaling laws for fully developed turbulent shear flows. Part 1. Basic hypotheses and analysis. J. Fluid Mech. 248, 513-520.
2. Cebeci, T., Smith, A.M.O., 1974. Analysis of Turbulent Boundary Layers. Academic Press, New York.
3. Clauser, F.H., 1954. Turbulent boundary layers in adverse pressure gradients. J. Aero. Sci. 21, 91-108.
4. Coles, D., 1956. The law of the wake in the turbulent boundary layer. J. Fluid Mech. 1, 191-226.
5. Dussauge, J.P., Smith, R.W., Smits, A.J., Fernholz, H., Finley, P.J., Spina, E.F., 1996. Turbulent boundary layers in subsonic and supersonic flow. Agardograph 335.
6. Fernholz, H.H., 1971. Ein halbempirisches Gesetz für due Wandreibung in kompressiblen turbulenten Grenzschichten bei isothermer und adiabater Wand. ZAMM 51, 146-147.
7. Fernholz, H.H., Finley, P.J., 1996. The incompressible zero-pressure-gradient turbulent boundary layer: An assessment of the data. Prog. Aerospace Sci. 32, 245-311.
8. 4 on the wall of the DNW. Phys. Fluids A 7, 1275-1281.
9. George, W.K., Knecht, P., Castillo, L., 1992. The zero-pressure gradient boundary layer revisited. In: Reed, X.B. (Ed.), Proceedings of Thirteenth Symposium on Turbulence, Rolla, Mo, USA.
10. Hanjalić, K., Jakirlić, S., Hadžić, I., 1995. Computation of oscillating turbulent flows at transitional Re-numbers. In: Durst, F. et al. (Eds.), Turbulent Shear Flows 9. Springer, Berlin, pp. 323-342.
11. Henkes, R.A.W.M., 1990. Natural-Convection Boundary Layers. Ph.D. Thesis, Delft University of Technology.
12. Henkes, R.A.W.M., 1997. Comparison of turbulence models for attached boundary layers relevant to aeronautics. Appl. Sci. Res. 57, 43-65.
13. Jakirlić, S., Hadžić, I., Hanjalić, K., 1994. Computation of non-equilibrium and separating flows at transitional and high Renumbers with a new low-Re-number second-moment closure model. In: Proceedings of Strömungen mit Ablösung, AGSTAB, DGLR Congress, Erlangen, Germany.
14. Launder, B.E., Sharma, B.I., 1974. Application of the energy-dissipation model of turbulence to the calculation of flow near a spinning disk. Lett. Heat Mass Transfer 1, 131-138.
15. Millikan, C.B., 1938. A critical discussion of turbulent flows in channels and circular tubes. In: Dentalartog, J.P., Peters, H. (Eds.), Proceedings of Fifth International Congr. of Appl. Mech., Cambridge, pp. 386-392.
16. Rotta, J.C., 1950. Über die Theorie der turbulenten Grenzschichten. Mitt, aus dem Max-Planck Inst, für Strömungsforschung, 1; also translated as: On the theory of the turbulent boundary layer. NACA TM 1344, 1953.
17. Rotta, J.C., 1950. Über die Theorie der turbulenten Grenzschichten. Mitt, aus dem Max-Planck Inst, für Strömungsforschung, 1; also translated as: On the theory of the turbulent boundary layer. NACA TM 1344, 1953.
18. 0 = 1410. J. Fluid Mech. 187, 61-98.
19. Tennekes, H., Lumley, J.L., 1972. A First Course in Turbulence. MIT Press, Cambridge, MA.
20. Townsend, A.A., 1976. The Structure of Turbulent Shear Flow. Cambridge University Press, Cambridge.
21. Von Kármán, T., 1930. Mechanische Ähnlichkeit und Turbulenz. Nachrichten der Konigliche Gesellschaft der Wissenschaften zu Göttingen, Math. Phys. Klasse, pp. 58-76.
22. Wilcox, D.C., 1993. Turbulence Modelling. DCW Industries Inc.
23. Winter, K.G., Gaudet, L., 1973. Turbulent boundary-layer studies at high Reynolds numbers at Mach numbers between 0.2 and 2.8. ARC R and M 3712.