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Numerical investigation of the effects of system volume and average mass flow on the surge characteristics of an axial compressor

  • Published:2020-11 Issue: Volume:106 Page:106172
  • ISSN:1270-9638
  • Container-title:Aerospace Science and Technology
  • language:en
  • Short-container-title:Aerospace Science and Technology

Author:

Wang Meng,Sun Haiou,Wang Zhongyi,Wang Yanhua,Magagnato Franco,Luan Yigang

Funder

National Natural Science Foundation of China

National Science and Technology Major Project

Outstanding Youth Foundation of Heilongjiang Province

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference28 articles.

1. A theory of post-stall transients in axial compression systems: part I—development of equations;Moore;J. Eng. Gas Turbines Power,1986

2. A theory of post-stall transients in axial compression systems: part II—application;Greitzer;J. Eng. Gas Turbines Power,1986

3. A hybrid approach for the modelling of axial compressor surge;Ananth;Int. J. Turbo Jet-Engines,2013

4. Dynamic model and simulation of compressor rotating stall and surge;Su;J. Propuls. Technol.,2016

5. Development and validation of a 1D model for turbocharger compressors under deep-surge operation;Bellis;Energy,2018

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