Effects of inert fuel diluents on the dynamic state of a thermoacoustically unstable gas turbine combustor (2019)
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/10.2514/6.2019-0672
Publication URI: http://dx.doi.org/10.2514/6.2019-0672
Type: Conference/Paper/Proceeding/Abstract