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TECHNICAL BRIEF

On the Momentum Balance in Linear-Combination Models for the Transition Zone

[+] Author and Article Information
J. Dey

Department of Aerospace Engineering, Indian Institute of Science, Bangalore 560012, India

J. Turbomach 122(3), 587-588 (Oct 01, 1997) (2 pages) doi:10.1115/1.1303704 History: Received October 01, 1997
Copyright © 2000 by ASME
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References

Cebeci, T., ed., 1983, Proc. Numerical Physical Aspects of Aerodynamic Flows II, Springer-Verlag, New York.
Mayle,  R. W., 1991, “The Role of Laminar–Turbulent Transition in Gas Turbine Engines,” ASME J. Turbomach., 113, pp. 509–537.
Narasimha,  R., and Dey,  J., 1989, “Transition Zone Models for 2-Dimensional Boundary Layers: A Review,” Sadhana, 14, pp. 93–120.
Dhawan,  S., and Narasimha,  R., 1958, “Some Properties of Boundary Layer During Transition From Laminar to Turbulent Motion,” J. Fluid Mech., 3, pp. 418–437.
Dey, J., and Narasimha, R., 1988, “An Integral Method for the Calculation of 2D Transitional Boundary Layers,” Dept. Aerospace Engg., Report 88FM7, Indian Institute of Science, Bangalore.
Dey,  J., and Narasimha,  R., 1990, “Integral Method for the Calculation of Incompressible Two-Dimensional Transitional Boundary Layer,” J. Aircr., 27, pp. 859–865.
Singer, B. A., and Dinavahi, S. P., 1991, “Testing of Transition Region Models: Test Cases and Data,” NASA CR 4371.
Gostelow, J. P., Hong, G., Walker, G. J., and Dey, J., 1994, “Modelling of Boundary Layer Transition in Turbulent Flow by Linear Combination Integral Method,” ASME Paper No. 94-GT-358.
Thwaites,  B., 1949, “Approximate Calculation of the Laminar Boundary Layer,” Aeronaut. Quart., 1, pp. 245–280.
Schubauer, G. B., and Klebanoff, P. S., 1955, “Contributions on the Mechanics of Boundary Layer Transition,” NACA TN 3489.
Narasimha,  R., 1957, “On the Distribution of Intermittency in the Transition Region of a Boundary Layer,” J. Aeronaut. Sci., 24, pp. 711–712.
Green, J. E., Weeks, D. J., and Brooman, J. W. F., 1973, “Prediction of Turbulent Boundary Layers and Wakes in Compressible Flow by Lag-Entrainment Method,” Royal Aircraft Establishment, Tech. Report 72231, Farnborough, UK.
Dey, J., 1998, “On the Momentum Balance in Linear Combination Models for the Transition Zone,” Dept. Aerospace Engg., Report 98FM7, Indian Institute of Science, Bangalore.

Figures

Grahic Jump Location
Variation of I1,I2, and momentum residual for the velocity distribution (1)
Grahic Jump Location
(a) Idealized velocity fluctuations due to a turbulent spot; (b) momentum residual for the velocity distribution (7)

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