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...

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Bibliographic Details
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
Other Authors: Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
Format: Article
Language:en_US
Published: ASME International 2017
Online Access:http://hdl.handle.net/1721.1/109142
https://orcid.org/0000-0002-4140-199X
https://orcid.org/0000-0003-2167-9860