Effect of Casing Groove Locations on the Performance of an Axial Flow Stage
Author:
Affiliation:
1. University of Tennessee, Chattanooga
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2013-3632
Reference36 articles.
1. 1Moore, R. D. "Rotor tip clearance effects on overall and blade-element performance of axial-flow transonic fan stage," NASA TN-D-6538.1982.
2. VKI Lecture Series;Freeman C.,1985
3. Three-Dimensional Flowfields Inside a Transonic Compressor With Swept Blades
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