Numerical prediction of the Flame Describing Function and thermoacoustic limit cycle for a pressurised gas turbine combustor (2019)
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/10.1080/00102202.2019.1583221
Publication URI: http://dx.doi.org/10.1080/00102202.2019.1583221
Type: Journal Article/Review
Parent Publication: Combustion Science and Technology
Issue: 5-6