Advanced application of a sublayer fence probe in highly instationary turbomachinery flows: observations on prestall instabilities

Author:

Eck Mario,Rückert Roland,Peitsch Dieter

Publisher

Springer Science and Business Media LLC

Subject

Fluid Flow and Transfer Processes,General Physics and Astronomy,Mechanics of Materials,Computational Mechanics

Reference28 articles.

1. Baumgartner M, Kameier F, Hourmouziadis J (1995) Non-engine order blade vibration in a high pressure compressor. In: Twelfth international symposium on airbreathing engines, Melbourne, Australia. https://hal.archives-ouvertes.fr/hal-01353829 , https://hal.archives-ouvertes.fr/hal-01353829/file/isabeb.pdf

2. Beselt Ch, van Rennings R, Thiele F, Peitsch D (2012) Experimental and numerical investigation of rotating instability phenomenon in an axial compressor stator. In: 42nd AIAA fluid dynamics conference and exhibit 2012. https://doi.org/10.2514/6.2012-2980

3. Beselt Ch, Pardowitz B, van Rennings R, Sorge R, Peitsch D, Enghardt L, Thiele F, Ehrenfried K, Thamsen P-U (2013a) Influence of the clearance size on rotating instability in an axial compressor stator. In: Proceedings of 10th European turbomachinery conference, No. ETC2013-141, Lappeenranta, Finland, 15–19 April 2013

4. Beselt C, Peitsch D, van Rennings R, Thiele F (2013b) Impact of hub clearance on endwall flow in a highly loaded axial compressor stator. In: ASME Turbo Expo 2013: turbine technical conference and exposition, number GT2013-95463. San Antonio (3–7 June 2013)

5. Beselt Ch, Eck M, Peitsch D (2014) Three-dimensional flow field in highly loaded compressor cascade. J Turbomach 136(10):10 (101007)

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