The nature of wakes in multistage axial flow compressors
Author:
Affiliation:
1. Rolls-Royce Aero Engines plc Derby, UK
2. Cranfield University Department of Turbomachinery and Engineering Mechanics, School of Mechanical Engineering Bedford, UK
Abstract
Publisher
SAGE Publications
Subject
Mechanical Engineering,Energy Engineering and Power Technology
Link
http://journals.sagepub.com/doi/pdf/10.1243/0957650991537617
Reference9 articles.
1. Unsteady Transition in an Axial-Flow Turbine: Part 1—Measurements on the Turbine Rotor
2. M. J. Hartmann Memorial Session Paper: Turbulence Characteristics in a Supersonic Cascade Wake Flow
3. The Measurement of Boundary Layers on a Compressor Blade in Cascade: Part 3—Pressure Surface Boundary Layers and the Near Wake
Cited by 2 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. Converged statistics for time-resolved measurements in low-speed axial fans using high-frequency response probes;Experimental Thermal and Fluid Science;2014-04
2. Non-deterministic kinetic energy within the rotor wakes and boundary layers of low-speed axial fans: frequency-based decomposition of unforced unsteadiness and turbulence;Journal of Turbulence;2009-01
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