Approximate Nonlinear Modeling of Aircraft Engine Surge Margin Based on Equilibrium Manifold Expansion
Author:
Publisher
Elsevier BV
Subject
Mechanical Engineering,Aerospace Engineering
Reference28 articles.
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4. A theory of post-stall transients in axial compression systems-Part II: application;Greitzer;ASME Journal of Engineering for Gas Turbines and Power,1986
5. Modeling for control of rotating stall in high-speed multistage axial compressors;Feulner;ASME Journal of Turbomachinery,1996
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