An experimental study of subcritical transition into thermoacoustic oscillations in a swirl stabilized model gas turbine combustor (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/10.2514/6.2020-1357
Publication URI: http://dx.doi.org/10.2514/6.2020-1357
Type: Conference/Paper/Proceeding/Abstract