Literature cited
L. V. Gogish and G. Yu. Stepanov, Turbulent Separated Flows [in Russian], Nauka, Moscow (1979).
J. E. Carter, “Solutions for laminar boundary layers with separation and reattachment,” AIAA Paper, No. 583 (1974).
H. McDonald and W. R. Briley, “A survey of recent work on interacting boundary-layer theory for flow with separation,” in: Numerical and Physical Aspects of Aerodynamic Flows. Vol. II, Springer, New York-Berlin (1984).
V. N. Vatsa and J. M. Verdon, “Viscid/inviscid interaction analysis of separted trailingedge flows,” AIAA J.,23, No. 4 (1985).
Aerodynamic Theory of Separated Flows [in Russian], Nauka, Moscow (1987).
J. O. Hinze, Turbulence, McGraw-Hill, New York (1959).
T. A. Reyhner and I. Flugge-Lotz, “The interaction of a shock wave with a laminar boundary layer,” Int. J. Non-Linear Mech.,3, No. 2 (1968).
A. A. Samarskii, Theory of Difference Scheme [in Russian], Nauka, Moscow (1977).
J. Blotner, “Difference scheme with a nonuniform grid to calculate turbulent boundary layers,” in: Numerical Solution of Problems of Fluid Mechanics [Russian translation], Mir, Moscow (1977).
G. N. Abramovich, S. Yu. Krasheninnikov, and A. P. Sekundov, Turbulent Flows in the Interaction of Body Forces and Non-Similitude [in Russian], Mashinostroenie, Moscow (1975).
R. L. Simpson, Y. T. Chew, and B. G. Shivaprasad, “The structure of separating turbulent boundary layer. Pt. I. Mean flow and Reynolds stresses,” J. Fluid Mech.,113, 23 (1981).
A. Halim and M. Hafez, “Calculation of separation bubbles using boundary-layer type equations,” AIAA J.,24, No. 4 (1986).
J. M. Serpa, R. C. Lessman, and W. M. Hagist, “Turbulent separated and reattached flows over a curved surface,” AIAA Paper, No. 1064 (1985).
Author information
Authors and Affiliations
Additional information
Translated from Zhurnal Prikladnoi Mekhaniki i Tekhnicheskoi Fiziki, No. 6, pp. 46–54, November–December, 1990.
Rights and permissions
About this article
Cite this article
Vasil'ev, V.I., Khokhlov, S.V. & Shal'man, E.Y. Calculation of separated flows by means of boundary-layer equations. J Appl Mech Tech Phys 31, 839–847 (1990). https://doi.org/10.1007/BF00854195
Received:
Revised:
Issue Date:
DOI: https://doi.org/10.1007/BF00854195