Unsteady Euler analysis of the redistribution of an inlet temperature distortion in a turbine
Author:
Affiliation:
1. United Technologies Corp., Pratt and Whitney Group, East Hartford, CT
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1990-2262
Reference15 articles.
1. Effects of Inlet Temperature Gradients on Turbomachinery Performance
2. Intra-Stator Transport of Rotor Wakes and Its Effect on Compressor Performance
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