Performance of an Axial Cascade
Basharat Salim
King Saud University, Riyadh, KSA.
DOI: 10.4236/ojfd.2013.33024   PDF    HTML   XML   7,667 Downloads   11,828 Views   Citations

Abstract

A cascade is defined as an infinite row of equidistant similarly aerofoil bodies. The cascade is used to divert a flow stream with a minimal loss. The flow over an axial cascade presents a complicated intra blade fluid dynamic interaction that causes the flow to behave differently than the flow over a single aerofoil blade. A cascade tunnel in which different shapes of cascades could be tested for performance evaluation has been build. An axial flat plate cascade of 70 mm chord, 215 mm span and 0.55 pitch chord ratio has been tested in this tunnel for evaluating its aerodynamic performance. The results depict that the Reynolds number, incidence and blade angle of the cascade control the aerodynamic performance of the axial cascade.

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B. Salim, "Performance of an Axial Cascade," Open Journal of Fluid Dynamics, Vol. 3 No. 3, 2013, pp. 191-197. doi: 10.4236/ojfd.2013.33024.

Conflicts of Interest

The authors declare no conflicts of interest.

References

[1] W. H. Roundebush, “Potential Flow in Two Dimensional Cascades, Chapter IV of ‘Aerodynamic Design of Axial Flow Compressors’,” NASA Sp 36, US Government Printing Office, Washington DC, 1965.
[2] N. Scholz, “Aerodynamics of Cascades,” AGARDograph No. 220, Nato Science and Technology Organization, Amsterdam, 1977.
[3] J. P. Gostlow, “Cascade Aerodynamics,” Pergaman Press, Oxford, 1984.
[4] N. A. Cumpsty, “Compressor Aerodynamics,” Longman Scientific and Technical, England, 1989.
[5] A. Felix and J. Emery, “A Comparison of Typical NGTE and NACA Axial Blade Compressor Blade Sections in Cascades at Low Speeds,” NACA TN 3937, US Government Printing Office, Washington DC, 1957.
[6] I. D. Baciu, “A S Profile Axial Cascade Tested in a Wind Tunnel,” International Conference on Hydraulic Machinery and Equipment, Timosoars, 16-17 October 2008, pp 45-48.
[7] S. J. Andrew, “Tests Related to the Effect of Profile Shape and Camber-Line on Compressor Cascade Performance,” Aeronautical Research Council R&M 2743, Aeronautical Research Council, England, 1949.
[8] G. Serovy, P. Kavanagh and T. Okishi, “Aerodynamics of Advanced Axial Turbomachinery,” NTIS Report ADA 131360, US Government Printing Office, Washington DC, 1983.
[9] G. Pullen and N. Harrvey, “Influence of Sweep on the Axial Flow Turbine Cascade at Mid Span,” Transactions of ASME, Journal of Turbomachinery, Vol. 129, No. 3, 2007.
[10] D. Kalpatrik and R. Burrow, “Aspect Ratio Effects on Compressor Cascade Blade Flutter,” ARC Technical Report, R&M No. 3103, Aeronautical Research Council, England, 1958.
[11] H. Mustaphe, D. Jourim and S. A. Scolander, “Aerodynamic Performance of a Transonic Turbine Cascade at Off Design Conditions,” Journal of Turbomachines, Vol. 123, No. 3, 2001, pp. 510-519.
[12] T. Nagasaki and N. Yamasaki, “Linear Unsteady Aerodynamic Forces on a Vibrating Annular Cascade Blade,” Journal of Thermal Sciences, Vol. 12, No. 2, 2003, pp. 138-143.
[13] R. Lanzafame and M. Messina, “Fluid Dynamic Wind Turbine Design: Critical Analysis, Optimization and Application of BEM Theory,” Renewable Energy, Vol. 32, No. 14, 2007, pp. 2291-2305.
[14] Mcormik and Barnes “Aerodynamics, Aeronautics and Flight Mechanics,” John Wiley and Sons, New York, 1979.

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