The effect of the finite extent of a linear cascade on the acoustic and vortical modes generated at the cascade exit by a set of moving bars located at the inlet is assessed by means of a numerical study. The sidewall interference is studied for an airfoil, which is representative of the midsection of a low pressure turbine airfoil. The deviations from the purely periodic steady state have been also investigated. It is concluded that both the unsteady pressure distributions on the airfoil and the mode-decomposition at the cascade exit show a reasonable matching with the purely periodic case, provided that the nominal interblade phase angle is taken into account to postprocess the numerical data. This conclusion is a key element to the investigation of the scattering and propagation of pure tones in turbomachinery in high speed linear cascades.
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e-mail: manuel.burgos@upct.es
e-mail: roque.corral@itp.es
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January 2011
Research Papers
Numerical Assessment of the Noise Signature Sidewall Contamination of a Linear Cascade With Moving Bars
Manuel A. Burgos,
Manuel A. Burgos
Department of Fluid Dynamics,
e-mail: manuel.burgos@upct.es
Universidad Politécnica de Cartagena
, 30203 Cartagene, Spain
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Roque Corral
Roque Corral
Department of Technology and Methods,
e-mail: roque.corral@itp.es
Industria de Turbo Propulsores S.A.
, 28830 Madrid, Spain
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Manuel A. Burgos
Department of Fluid Dynamics,
Universidad Politécnica de Cartagena
, 30203 Cartagene, Spaine-mail: manuel.burgos@upct.es
Roque Corral
Department of Technology and Methods,
Industria de Turbo Propulsores S.A.
, 28830 Madrid, Spaine-mail: roque.corral@itp.es
J. Turbomach. Jan 2011, 133(1): 011006 (10 pages)
Published Online: September 9, 2010
Article history
Received:
July 29, 2008
Revised:
February 13, 2009
Online:
September 9, 2010
Published:
September 9, 2010
Citation
Burgos, M. A., and Corral, R. (September 9, 2010). "Numerical Assessment of the Noise Signature Sidewall Contamination of a Linear Cascade With Moving Bars." ASME. J. Turbomach. January 2011; 133(1): 011006. https://doi.org/10.1115/1.4000487
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