An Investigation of Stall Inception in Centrifugal Compressor Vaned Diffusers
In compression systems the stable operating range is limited by rotating stall and/or surge. Two distinct types of stall precursors can be observed prior to full scale instability: the development of long-wavelength modal waves or a shortwavelength, three-dimensional flow breakdown (so-called "...
Main Authors: | Everitt, Jonathan Neil, Spakovszky, Zoltan S |
---|---|
Other Authors: | Massachusetts Institute of Technology. Department of Aeronautics and Astronautics |
Format: | Article |
Published: |
ASME International
2018
|
Online Access: | http://hdl.handle.net/1721.1/116186 https://orcid.org/0000-0003-2167-9860 |
Similar Items
-
Investigation of stall inception in centrifugal compressors using isolated diffuser simulations
by: Everitt, Jonathan (Jonathan Neil)
Published: (2011) -
Stall and leading-edge vortex in a centrifugal compressor with vaned diffuser
by: Nobumichi FUJISAWA, et al.
Published: (2015-08-01) -
Investigation of Suction Flow Control on Centrifugal Compressor with Vaned Diffuser
by: Suleyman Emre Ak, et al.
Published: (2022-01-01) -
The Role of Impeller Outflow Conditions on the Performance of Vaned Diffusers
by: Rusch, Daniel, et al.
Published: (2018) -
The Role of Impeller Outflow Conditions on the Performance of Vaned Diffusers
by: Rusch, Daniel, et al.
Published: (2018)