Abstract
The flow of gas in a channel with division of the flow by a longitudinal baffle is characterized by the ratio m of the flow rates in the exterior (Ge) and interior (Gi) parts of the channel: m = Ge/Gi. For example, flow in a channel with a wall screen forming a narrow annular slit with the channel wall corresponds to m ≪ 1. In the case of a gas extraction pipe in the channel m ≪ 1. In two-profile gas turbine engines m is of the order of unity or several units [1]. Flow in a channel with a baffle is characterized by the presence of a “liquid” boundary between the flows up to the start of the baffle. For given shape of the channel and baffle, the position of the separating stream surface depends on the conditions of the problem. In the present paper, the influence of the flow rate ratio m on the flow pattern in such a channel is investigated numerically.
Similar content being viewed by others
Literature cited
B. A. Ponomarev, Two-Profile Jet Turbine Engines [in Russian], Voenizdat, Mowcow (1973).
Ch. Hirsch and G. Warzee, “Finite-element method for through flow calculations in turbomachines,” Trans. Am. Soc. Mech. Eng., Ser. I, J. Fluids Eng.,96, 403 (1976).
S. K. Godunov and V. S. Ryaben'kii, Difference Schemes [in Russian], Nauka, Moscow (1973).
L. G. Loitsyanskii, Mechanics of Liquids and Gases, Pergamon Press, Oxford (1966).
Garret and Flugmotor Volvo, “TFE1042 low bypass turbofan,” Aviat. Week Space Technol.,110, No. 23 (1979).
Author information
Authors and Affiliations
Additional information
Translated from Izvestiya Akademii Nauk SSSR, Mekhanika Zhidkosti i Gaza, No. 4, pp. 154–156, July–August, 1981.
Rights and permissions
About this article
Cite this article
Konovalov, A.E. Calculations of subsonic inviscid flows in axisymmetric channels with division of the flow. Fluid Dyn 16, 617–620 (1981). https://doi.org/10.1007/BF01094611
Received:
Issue Date:
DOI: https://doi.org/10.1007/BF01094611