Fan Response to Boundary-Layer Ingesting Inlet Distortions
Author:
Affiliation:
1. The Ohio State University, Columbus, Ohio 43210
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J054762
Reference14 articles.
1. Wake ingestion propulsion benefit
2. Performance of a Boundary Layer Ingesting (BLI) Propulsion System
3. Effects of Inlet Distortion on Aeromechanical Stability of a Forward-Swept High-Speed Fan
4. ChimaR. V.ArendD. J.CastnerR. S.SlaterJ. W.TruaxP. P. “CFD Models of a Serpentine Inlet, Fan, and Nozzle,” NASA TM-2010-216349, May 2010.
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