Modeling of Coupled Open Rotor Engine Intakes
Author:
Affiliation:
1. University of Cambridge
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2010-840
Reference17 articles.
1. Aerodynamic Analysis of Multistage Turbomachinery Flows in Support of Aerodynamic Design
2. A Three-Dimensional Unsteady CFD Model of Compressor Stability
3. 1997 Best Paper Award—Education Committee: A Three-Dimensional Turbine Engine Analysis Compressor Code (TEACC) for Steady-State Inlet Distortion
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