3D flow around blades

Underlying Flow Regime 2-07 © copyright ERCOFTAC 2004

References

[1]	Wood, J. R., Strazisar, T., Hathaway M., Test Case E/CO-2 Single Transonic Fan Rotor, AGARD-Report, AR-275, pp 165-213, July 1990
[2]	Shabbir, A., Celestina, M.L., Adamczyk, J.J., Strazisar, A.J., The Effect of Hub Leakage Flow on Two High Speed Axial Flow Compressor Rotors, ASME International Gas Turbine and Aeroengine Congress and Exhibition, June 1997
[3]	Baldwin, B., Lomax, H., Thin Layer Approximation and Algebraic Model for Separated Turbulent Flows, AIAA Paper 78-257, Jan. 1978
[4]	Spalart, P. R., Allmaras, S. R., A One-Equation Turbulence Model for Aerodynamic Flows, AIAA Report 92-0439, Jan. 1992
[5]	Adamczyk, J. J., Celestina, M. L., Greitzer, E. M., The Role of Tip Clearance in High-Speed Fan Stall, Transactions of the ASME, Vol. 115, Jan. 1993, pp. 28-39
[6]	Cohen, H., Rogers, G. F. C., Saravanamuttoo, H. I. H., Gas Turbine Theory, Fourth Edition (1996), pp. 171
[7]	Jameson, A., Baker, T.J. “Multigrid Solution of the Euler Equations for Aircraft Configurations”, AIAA Paper 84-0093 (1984)
[8]	Pierzga, M.J., Wood, J.R., “Investigation of the Three-Dimensional Flow Field Within a Transonic Fan Rotor: Experiment and Analysis”, ASME Journal of Engineering for Gas Turbines and Power, Vol. 107, No.2, April 1985, pp. 436449.

Contributors: William Anderson - ALSTOM Power (Switzerland) Ltd