Aeromechanics Analysis of a Distortion-Tolerant Fan with Boundary Layer Ingestion
Author:
Affiliation:
1. NASA Glenn Research Center
2. University of Toledo
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-1891
Reference23 articles.
1. Wake ingestion propulsion benefit
2. Performance of a Boundary Layer Ingesting (BLI) Propulsion System
3. Hybrid Wing Body Configuration System Studies
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2. Conceptual aero-structural design of a fan stage under distorted flow;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2023-01-28
3. Aeromechanical Response of a Distortion-Tolerant Boundary Layer Ingesting Fan;Journal of Engineering for Gas Turbines and Power;2018-09-14
4. Laser Displacement Measurements of Fan Blades in Resonance and Flutter During the Boundary Layer Ingesting Inlet and Distortion-Tolerant Fan Test;2018 AIAA Aerospace Sciences Meeting;2018-01-07
5. Cyclic Symmetry Finite Element Forced Response Analysis of a Distortion Tolerant Fan with Boundary Layer Ingestion;2018 AIAA Aerospace Sciences Meeting;2018-01-07
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