Wake of a Compressor Cascade with Tip Gap, Part 2: Effects of Endwall Motion
Author:
Affiliation:
1. Virginia Polytechnic Institute and State University, Blacksburg, Virginia 24061
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.5272
Reference16 articles.
1. ‡Data available online at http://www.aoe.vt.edu/flowdata [cited 1 Oct. 2004].
2. The Effect of Tip Clearance Gap Size and Wall Rotation on the Performance of a High-Speed Annular Compressor Cascade
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