The momentum balance of the linear-combination integral model for the transition zone is investigated for constant pressure flows. The imbalance is found to be small enough to be negligible for all practical purposes. [S0889-504X(00)00703-0]

1.
Cebeci, T., ed., 1983, Proc. Numerical Physical Aspects of Aerodynamic Flows II, Springer-Verlag, New York.
2.
Mayle
,
R. W.
,
1991
, “
The Role of Laminar–Turbulent Transition in Gas Turbine Engines
,”
ASME J. Turbomach.
,
113
, pp.
509
537
.
3.
Narasimha
,
R.
, and
Dey
,
J.
,
1989
, “
Transition Zone Models for 2-Dimensional Boundary Layers: A Review
,”
Sadhana
,
14
, pp.
93
120
.
4.
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
.
5.
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.
6.
Dey
,
J.
, and
Narasimha
,
R.
,
1990
, “
Integral Method for the Calculation of Incompressible Two-Dimensional Transitional Boundary Layer
,”
J. Aircr.
,
27
, pp.
859
865
.
7.
Singer, B. A., and Dinavahi, S. P., 1991, “Testing of Transition Region Models: Test Cases and Data,” NASA CR 4371.
8.
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.
9.
Thwaites
,
B.
,
1949
, “
Approximate Calculation of the Laminar Boundary Layer
,”
Aeronaut. Quart.
,
1
, pp.
245
280
.
10.
Schubauer, G. B., and Klebanoff, P. S., 1955, “Contributions on the Mechanics of Boundary Layer Transition,” NACA TN 3489.
11.
Narasimha
,
R.
,
1957
, “
On the Distribution of Intermittency in the Transition Region of a Boundary Layer
,”
J. Aeronaut. Sci.
,
24
, pp.
711
712
.
12.
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.
13.
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.
You do not currently have access to this content.