Computational simulations of a multi-stage subsonic research compressor

Kidambi Sreenivas, Robert S. Webster, Ethan A. Hereth, Reid A. Berdanier, Nicole L. Key

Research output: Chapter in Book/Report/Conference proceedingConference contribution

1 Scopus citations

Abstract

The machine that is the subject of this work has been used for numerous experimental studies over a number of years. It is representative of the aft stages of a core compressor in which the flow is entirely subsonic. The experimental studies have been primarily focused on vane clocking and the related effects on compressor performance, as well as stall margin; a multi-year study was recently completed, which looked at tip-clearance effects. This paper is, on the other hand, an entirely computational effort that will make use of the extensive experimental database associated with this machine in order to validate the numerical results. The plan will then be to conduct further fundamental aerodynamic research in a collaborative experimental/computational setting. The results are encouraging, but they should be taken as preliminary in their context.

Original languageEnglish (US)
Title of host publication54th AIAA Aerospace Sciences Meeting
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)9781624103933
DOIs
StatePublished - Jan 1 2016
Event54th AIAA Aerospace Sciences Meeting, 2016 - San Diego, United States
Duration: Jan 4 2016Jan 8 2016

Publication series

Name54th AIAA Aerospace Sciences Meeting
Volume0

Other

Other54th AIAA Aerospace Sciences Meeting, 2016
CountryUnited States
CitySan Diego
Period1/4/161/8/16

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering

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    Sreenivas, K., Webster, R. S., Hereth, E. A., Berdanier, R. A., & Key, N. L. (2016). Computational simulations of a multi-stage subsonic research compressor. In 54th AIAA Aerospace Sciences Meeting (54th AIAA Aerospace Sciences Meeting; Vol. 0). American Institute of Aeronautics and Astronautics Inc, AIAA. https://doi.org/10.2514/6.2016-0395