Unsteady Flow and Whirl-Inducing Forces in Axial-Flow Compressors: Part II-Analysis

Unsteady Flow and Whirl-Inducing Forces in Axial-Flow Compressors: Part II-Analysis

An experimental and theoretical investigation was conducted to evaluate the effects seen in axial-flow compressors when the centerline of the rotor becomes displaced from the centerline of the static structure of the engine, thus creating circumferentially nonuniform rotor-tip clearances. This displ...

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Bibliographic Details
Main Authors: Song, S. J. (Author), Wisler, D. C. (Author), Storace, A. F. (Author), Shin, H.-W (Author), Beacher, B. F. (Author), Ehrich, Fredric F (Contributor), Spakovszky, Zoltan S (Contributor), Martinez-Sanchez, Manuel (Contributor)
Other Authors: Massachusetts Institute of Technology. Department of Aeronautics and Astronautics (Contributor)
Format: Article
Language:English
Published: ASME International, 2017-01-09T14:53:22Z.
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