Aircraft Engine Surge-Precursor Detection and Antisurge Control Method at Onboard Environment
Author:
Affiliation:
1. Nanjing University of Aeronautics and Astronautics, 21006 Nanjing, People’s Republic of China
Funder
National Natural Science Foundation of China
Aviation Science Foundation of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J061403
Reference24 articles.
1. Stall and Surge Precursors in Axial Compressors
2. Flow Stability Model of Centrifugal Compressors Based on Eigenvalue Approach
3. Throttling Process and Buzz Mechanism of a Supersonic Inlet at Overspeed Mode
4. Comparison and Sensibility Analysis of Warning Parameters for Rotating Stall Detection in an Axial Compressor
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