Experimental Study on Linear Compressor Cascade with Three-Dimensional Blade Oscillation
Author:
Affiliation:
1. University of Durham, Durham, England, DH1 3LE, United Kingdom
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/10.2514/1.1280
Reference20 articles.
1. Experimentally Determined Stability Parameters of a Subsonic Cascade Oscillating Near Stall
2. Effect of Interblade Phase Angle and Incidence Angle on Cascade Pitching Stability
3. Unsteady Flow in Oscillating Turbine Cascades: Part 1—Linear Cascade Experiment
4. Oscillating Cascade Aerodynamics at Large Mean Incidence
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