Computational Inlet Swirl Distortion Investigation of a High-Speed Compressor
Author:
Affiliation:
1. Wright State University
2. Air Force Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Reference14 articles.
1. A Methodology for Assessing Inlet Swirl Distortion, Aerospace Information Report 5686, Society of Automotive Engineers, Inc., July, 2017.
2. An experimental investigation of the flow in a diffusing S-duct
3. Demonstration of a Remotely-Controlled Swirl Generator for Simulating Aircraft Inlet Secondary Flows During Turbine Engine Ground Tests
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1. Detached-Eddy Simulation and Swirl Distortion Characterization of an S-Duct Inlet;Arabian Journal for Science and Engineering;2022-07-17
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