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Thermoacoustic limit cycle predictions of a pressurised longitudinal industrial gas turbine combustor (2018)

First Author: Xia Y.

Attributed to: HIGH PERFORMANCE COMPUTING SUPPORT FOR UNITED KINGDOM CONSORTIUM ON TURBULENT REACTING FLOWS (UKCTRF) funded by EPSRC

Abstract

No abstract provided

Bibliographic Information

Digital Object Identifier: http://dx.doi.org/10.1115/gt201875146

Publication URI: http://dx.doi.org/10.1115/gt201875146

Type: Other

Volume: 4A-2018

Parent Publication: Proceedings of the ASME Turbo Expo