Gas Turbine Engine Fan Blade Flutter Detection Using Casing Vibration Signals by Application of Recurrence Plots and Recurrence Quantification Analysis

Author:

Viswanatha Rao A. N.,Naidu V. P. S.,Jana Soumendu

Publisher

Springer Singapore

Reference14 articles.

1. Technology Focus Gas Turbine Research Bulletin of Defence Research and Development Organisation DRDO, Ministry of Defence, India, vol 17, no 5 October 2009. ISSN 0971-4413

2. Srinivasan AV (1997) Flutter and resonant vibration characteristics of engine blades. In: AnIGTI scholar paper, 97-GT-533, Presented at the international gas turbine &aero engine congress & exhibition, Orlando, FL 2–5 June 1997

3. Purushotaman K, Jeyaraman SK, Pratap A, Deshkulakarni KP (2017) Aeroelastic flutter investigation and stability enhancement of a transonic axial compressor rotor using casing treatment. In: Paper No. GTINDIA 2017–4767, pp V001 T0 1A015, https://doi.org/10.1115/gtindia2017-4767 presented during ASME 2017 gas turbine india conference, Bangalore, India, 7–8 Dec 2017. ISBN 978-0-7918-5850-9

4. Viswanatha Rao AN et al. Challenges in engine health monitoring instrumentation during developmental testing of gas turbine engines. In: Paper no 153, proceedings of the 2nd national aero propulsion conference, NAPC-2018 7–19 Dec 2018, IIT Kharagpur, West Bengal (proceedings yet to be released)

5. Riazet S et al (2017) Vibration feature extraction and analysis for fault diagnosis of rotating machinery—A literature survey. Asia Pac J Multi Research 5(1):103–110

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