Circumferential Structure of Rotating Instability under Variation of Flow Rate and Solidity

VDI Berichte

Volumn , Issue 1425, 1998, Pages 189-198

  Marz J ^a   Neuhaus, L ^a   Neise, W ^a   Gui, X ^a  

^a NONE

Author keywords

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Indexed keywords

EID: 2542609322     PISSN: 00835560     EISSN: None     Source Type: Book Series    
DOI: None     Document Type: Article

References (8)

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2. M. Baumgartner, F. Kameier and J. Hormouziadis: Non engine order blade vibration in a high speed compressor. Twelfth International Symposium on Airbreathing Engines, Melbourne, Australia, 10.-15. Sept. 1995
3. R. Müller, R. Mailach: Experimentelle Untersuchung von Verdichterinstabilitäten am Niedergeschwindigkeitsverdichter Dresden, VDI-GET-Tagung Turbokompressoren im industriellen Einsatz, Hannover, Oktober 1998
4. nd AIAA/CEAS Aeroacoustics Conference, 1996
5. L. Neuhaus: Einfluβ der Schaufelzahl auf die azimutale Modenstruktur des Blattspitzen-Wirbellärms einer axialen Strömungsmaschine, diploma thesis, Technische Universität Berlin, 1996
6. J.M. Tyler and T.G. Sofrin: Axial Flow Compressor Noise Studies, SAE Transactions 70, 1962, p. 309-332
7. D.A. Hoying: Blade Passage Flow Structure Effects on Axial Compressor Rotating Stall Inception, Ph.D. Dissertation, 1996, Dept. Of Aeronautics and Astronautics, M.I.T.
8. ISO 5136 Determination of sound power radiated into a duct by fans - In-duct method. 1990 International Standard, International Organisation for Standardization.