Unsteady hot streak simulation through a 1-1/2 stage turbine engine
Author:
Affiliation:
1. Pratt and Whitney Group, East Hartford, CT
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1991-3382
Reference15 articles.
1. Unsteady Euler analysis of the redistribution of an inlet temperature distortion in a turbine
2. Unsteady analysis of hot streak migration in a turbine stage
3. Effects of Inlet Temperature Gradients on Turbomachinery Performance
4. Intra-Stator Transport of Rotor Wakes and Its Effect on Compressor Performance
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