Unsteady Flow and Whirl-Inducing Forces in Axial-Flow Compressors: Part I—Experiment
An experimental and theoretical investigation has been conducted to evaluate the effects seen in axial-flow compressors when the centerline of the rotor is displaced from the centerline of the static structure of the engine. This creates circumferentially nonuniform rotor-tip clearances...
Main Authors: | Storace, A. F., Wisler, D. C., Shin, H.-W., Beacher, B. F., Song, S. J., Ehrich, Fredric F, Spakovszky, Zoltan S, Martinez-Sanchez, Manuel |
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Other Authors: | Massachusetts Institute of Technology. Department of Aeronautics and Astronautics |
Format: | Article |
Language: | en_US |
Published: |
ASME International
2017
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Online Access: | http://hdl.handle.net/1721.1/109142 https://orcid.org/0000-0002-4140-199X https://orcid.org/0000-0003-2167-9860 |
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