A Modified Circumferentially Averaged Method for Compressor Performance under Inlet Distortion
Author:
Affiliation:
1. Aeroengine Simulation Research Center, School of Energy and Power Engineering, Beihang University, Beijing 100191, China
2. Jiangxi Research Institute, Beihang University, Nanchang 330096, China
Abstract
Publisher
MDPI AG
Subject
Aerospace Engineering
Link
https://www.mdpi.com/2226-4310/10/3/207/pdf
Reference27 articles.
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3. Schmollgruber, P., Donjat, D., Ridel, M., Cafarelli, I., Atinault, O., François, C., and Paluch, B. (2020, January 6). Multidisciplinary Design and performance of the ONERA Hybrid Electric Distributed Propulsion concept (DRAGON). Proceedings of the AIAA Scitech 2020 Forum, Orlando, FL, USA.
4. Medic, G., You, D., Kalitzin, G., Herrmann, M., and Alonso, J. (2007, January 14–17). Integrated Computations of an Entire Jet Engine. Proceedings of the Asme Turbo Expo: Power for Land, Sea, & Air, Montreal, QC, Canada.
5. Benichou, E., Binder, N., Bousquet, Y., and Carbonneau, X. (2021). Improvement of the Parallel Compressor Model and Application to Inlet Flow Distortion. Int. J. Turbomach. Propuls. Power, 6.
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