Extinction strain rate suppression of the precessing vortex core in a swirl stabilised combustor and consequences for thermoacoustic oscillations (2020)
Attributed to:
Advanced Gas Turbine cycles for high efficiency and sustainable future conventional generation
funded by
EPSRC
Abstract
No abstract provided
Bibliographic Information
Digital Object Identifier: http://dx.doi.org/10.1016/j.combustflame.2019.09.031
Publication URI: http://dx.doi.org/10.1016/j.combustflame.2019.09.031
Type: Journal Article/Review
Parent Publication: Combustion and Flame