A Novel Approach to Evaluate the Benefits of Casing Treatment in Axial Compressors
Author(s) -
Guillaume Legras,
Isabelle Trébinjac,
Nicolas Gourdain,
Xavier Ottavy,
Lionel Castillon
Publication year - 2012
Publication title -
international journal of rotating machinery
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.265
H-Index - 33
eISSN - 1026-7115
pISSN - 1023-621X
DOI - 10.1155/2012/975407
Subject(s) - casing , transonic , axial compressor , rotational symmetry , gas compressor , rotor (electric) , flow (mathematics) , current (fluid) , mechanics , mechanical engineering , computer science , blade (archaeology) , structural engineering , engineering , physics , aerodynamics , electrical engineering
Passive control devices based on casing treatments have already shown their capability to improve the flow stability in axial compressors. However, their optimization remains complex due to a partial understanding of the related physical mechanisms. In order to quantitatively assess the interaction between slots and the blade tip flow, the present paper develops a novel analysis methodology based on a control-volume approach located in the rotor tip region. This methodology may be used for analyzing the casing treatment based on both axi- and non-axisymmetric slots design. The second issue of the paper focuses on the application of the current approach to better understand the effects of axi- and non-axisymmetric grooves in three different axial compressors which differ by the flow regime (subsonic/transonic) and the smooth casing shape (cylindrical/concave). Numerical simulations are performed, and results of the current approach with and without casing treatments are compared
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