Predicting the Performance of a Gas Turbine Engine Undergoing Compressor Blade Erosion
Author:
Affiliation:
1. Concurrent Technologies Corporation
2. U.S. Army Industrial Ecology Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2003-5259
Reference30 articles.
1. Pressure Distribution on Blades in Cascade Nozzle for Particulate Flow
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