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