Experimental assessment on effect of lower porosities of bend skewed casing treatment on the performance of high speed compressor stage with tip critical rotor characteristics-Reference-Cited by-同舟云学术

Experimental assessment on effect of lower porosities of bend skewed casing treatment on the performance of high speed compressor stage with tip critical rotor characteristics

Published:2017-01 Issue: Volume:60 Page:193-202
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Alone Dilipkumar Bhanudasji,Kumar S. Satish,Shobhavathy M.T.,Mudipalli Janaki Rami Reddy,Pradeep A.M.,Ramamurthy Srinivasan,Iyengar Venkat S.

Funder

CSIR

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference18 articles.

1. A fundamental criterion for the application of rotor casing treatment;Greitzer;J. Fluids Eng.,1979

2. Experimental and numerical investigation of a subsonic compressor with bend-skewed slot-casing treatment;Lu;Proc. Inst. Mech. Eng., Part C, J. Mech. Eng. Sci.,2006

3. The stability-limiting in a subsonic axial flow compressor and its passive control with casing treatment;Lu,2008

4. Numerical investigations of the coupled flow through a subsonic compressor rotor and axial skewed slot;Lu;J. Turbomach.,2009

5. The effect of a bend-slot casing treatment on the blade tip flow field of a transonic compressor rotor, GT2013-94006;Voges,2013

Cited by 22 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. An Evaluation of Passive Wall Treatment with Circumferential Grooves at the Casing of the First and Second Blade Rotor Rows of a High-Performance Multi-Stage Axial Compressor;Aerospace;2024-08-12

2. Numerical analysis of the effect of different positions of circumferential grooves casing treatment on the stability expansion of mixed flow pumps;Journal of Mechanical Science and Technology;2024-06

3. An Evaluation of Passive Wall Treatment With Circumferential Grooves at the Casing of the First and Second Blade Rotor Rows of a High-performance Multi-stage Axial Compressor;2023-12-27

4. The influence of a coupled casing on the performance of a multistage compressor under inlet distortion conditions;AIP Advances;2023-12-01

5. Evolution of unsteady secondary flow structures near the onset of stall in a tip-critical transonic axial flow compressor stage;Physics of Fluids;2023-10-01