A method of predicting the performance deterioration of a compressorcascade due to sand erosion
Author:
Affiliation:
1. Cincinnati, University, Cincinnati, OH
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1983-178
Reference20 articles.
1. Mechanisms of Sand and Dust Erosion in Gas Turbine Engines.
2. Measurements Concerning the Influence of Surface Roughness and Profile Changes on the Performance of Gas Turbines
3. Experimental and Analytical Investigation of the Effects of Reynolds Number and Blade Surface Roughness on Multistage Axial Flow Compressors
4. Emery, J.C., Herrig, L.J., Erwig, J.R. and Felix, A.R. "SystematicTWODimensional Cascade Tests of NACA-65 Series Compressor Blades at Low Speeds," NACA Report 1368.
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