Nonlinear models for a compressor stall phenomenon using a single pressure measurement

Author:

Mossayebi Faramarz D.ORCID,Qammar Helen K.

Funder

National Science Foundation

Publisher

Springer Science and Business Media LLC

Subject

General Earth and Planetary Sciences,General Physics and Astronomy,General Engineering,General Environmental Science,General Materials Science,General Chemical Engineering

Reference24 articles.

1. Kerrebrock JL (1987) Aircraft engines and gas turbines. MIT Press, Cambridge

2. Denton JD, Dawes WN (1990) Computational fluid dynamics for turbomachinery. Proc Inst Mech Eng Part C J Mech Eng Sci 213:107–124

3. Reed L, Moore RD (1978) Design and overall performance of four highly loaded, high-speed inlet stages for an advanced high-pressure ratio core compressor. NASA Technical Paper 1337

4. Moore RD, Reid L (1980) Performance of single-stage axial-flow transonic compressor with rotor and stator aspect ratios of 1.19 and 1.26, respectively, and with design pressure ratio of 2.05. NASA Technical Paper 1659

5. Schreiber T, Kantz H (2005) Nonlinear time series analysis, 2nd edn. Cambridge University Press, Cambridge

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