Experimental and Computational Methods for Flow Investigation in High-Speed Multistage Compressor
Author:
Affiliation:
1. École Centrale de Lyon, 69130 Ecully, France
2. European Centre for Research and Advanced Training in Scientific Computation, 31057 Toulouse, France
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.B34412
Reference39 articles.
1. Rotor-Stator Interactions in a Four-Stage Low-Speed Axial Compressor—Part I: Unsteady Profile Pressures and the Effect of Clocking
2. Unsteady Aerodynamic Blade Excitation at the Stability Limit and During Rotating Stall in an Axial Compressor
3. Multi-Blade Row Interactions in a Transonic Axial Compressor: Part I—Stator Particle Image Velocimetry (PIV) Investigation
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