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Novel Gas Turbine Fault Diagnosis Method Based on Performan..:
Li, Zhen
;
Zhong, Shi-Sheng
;
Lin, Lin
Journal of Propulsion and Power. 33 (2017) 3 - p. 730-739 , 2017
Link:
https://doi.org/10.2514/1.b36267
RT Journal T1 <Title>Novel Gas Turbine Fault Diagnosis Method Based on Performance Deviation Model</Title> UL https://suche.suub.uni-bremen.de/peid=cr-10.2514_1.b36267&Exemplar=1&LAN=DE A1 Li, Zhen A1 Zhong, Shi-Sheng A1 Lin, Lin PB American Institute of Aeronautics and Astronautics (AIAA) YR 2017 SN 0748-4658 SN 1533-3876 JF Journal of Propulsion and Power VO 33 IS 3 SP 730 OP 739 LK http://dx.doi.org/https://doi.org/10.2514/1.b36267 DO https://doi.org/10.2514/1.b36267 SF ELIB - SuUB Bremen
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