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...

Full description

Bibliographic Details
Main Authors: Song, S. J., Wisler, D. C., Storace, A. F., Shin, H.-W., Beacher, B. F., 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/1721.1/106282
https://orcid.org/0000-0002-4140-199X
https://orcid.org/0000-0003-2167-9860

Internet

http://hdl.handle.net/1721.1/106282
https://orcid.org/0000-0002-4140-199X
https://orcid.org/0000-0003-2167-9860

Similar Items