Investigation of the Shear Flow Effect on Secondary Flow and Losses in a Low Speed Axial Flow Compressor Cascade

Author:

Varpe Mahesh K.1,Pradeep A. M.1

Affiliation:

1. Department of Aerospace Engineering, Indian Institute of Technology, Bombay

Publisher

Gas Turbine Society of Japan

Subject

Mechanical Engineering

Reference25 articles.

1. Brandt H., Fottner L., Saathoff H. and Stark U., 2002, ”Effects of the Inlet Flow Conditions on the Tip Clearance Flow of an Isolated Compressor Rotor”, ASME Turbo Expo 2002: Power for Land, Sea, and Air , June 3–6, 2002, Amsterdam, The Netherlands, GT2002-30639.

2. Choi M., Oh S. H., Ko H.Y. and Baek H. J., 2008, ”Effects of the Inlet Boundary Layer Thickness on Rotating Stall in an Axial Compressor”, Proceedings of ASME Turbo Expo 2008: Power for Land, Sea and Air , June 9-13, Berlin, Germany, GT2008-50886.

3. De Vahl D.G., 1962, “The flow of air through wire screens,” Proc. 1st Australasian Conference on Hydraulics and Fluid Mechanics , pp.191–212.

4. Elder J.W., 1959, “Steady flow through non non-uniform gauzes of arbitrary shape,” J. Fluid Mech , Vol. 5, pp.355-368.

5. Germain T, Nagel M and Baier R. D., 2007, “Visualisation and quantification of secondary flows: Application to turbine bladings with 3D-endwalls,” Proceedings of the 8th International Symposium on Experimental and Computational Aerothermodynamics of Internal Flows , Lyon, ISAIF8-0098 pp.1-10.

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