Effect of system response on partial surge initiated instability in a transonic axial flow compressor

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Unsteady Transonic Flows in an Axial Flow Compressor*

Introduction. This paper deals with some transonic flow problems for the supersonic axial flow compressor: these arise in connection with flutter analysis for fan blading. Very detailed solutions for unsteady plane transonic flows through a cascade of flat plates have been given by Goldstein Braun and Adamczyk (1977) and Nagashima and Whitehead (1977), see also Goldstein (1975), Kurosaka (1974)...

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ژورنال

عنوان ژورنال: Chinese Journal of Aeronautics

سال: 2021

ISSN: 1000-9361

DOI: 10.1016/j.cja.2020.12.043