Interpretation of stall precursor signatures-stable instabilities

¹ Université de Lyon, Ecole Centrale de Lyon, CNRS, LMFA, UMR 5509, F-69134, ECULLY, France
² Imperial College, Department of Mechanical Engineering, London, United Kingdom

^* Christoph Brandstetter: christoph.brandstetter@ec-lyon.fr
^† Xavier Ottavy: xavier.ottavy@ec-lyon.fr
^‡ Sina Stapeldeldt: s.stapelfeldt@imperial.ac.uk

Abstract

A specific phenomenon that has been observed in many experimental studies on turbomachinery compressors and fans is discussed under the term “rotating instabilities”. It is associated to a local aerodynamic phenomenon, typically occurring in the tip region at highly loaded near stall conditions and often linked to blade vibrations. Even though the effect has been discussed over more than two decades, a very ambiguous interpretation still prevails. A particular problem is that certain signatures in measurement data are often considered to characterize the phenomenon despite possible misinterpretations. The present paper illustrates that a specific image of a pulsating disturbance that has been established in the 1990s needs to be reconsidered. At the example of a recent investigation on a composite fan the difficulties concerning sensor placement and post-processing techniques is discussed with a focus on spectral averaging, isolation of non-synchronous phenomena and multi-sensor cross-correlation methods.