The identification and prediction of helical modes induced by a multi-passage swirl stabilised lean burn aero-engine fuel injector under steady state and acoustically forced conditions (2018)
Attributed to:
A MIDLANDS CENTRE OF EXCELLENCE FOR HIGH PERFORMANCE COMPUTING (HPC) SERVING REGIONAL INDUSTRY AND ACADEMIA - 'HPC MIDLANDS'
funded by
EPSRC
Abstract
No abstract provided
Bibliographic Information
Digital Object Identifier: http://dx.doi.org/10.1115/gt201875552
Publication URI: http://dx.doi.org/10.1115/gt201875552
Type: Other
Volume: 4A-2018
Parent Publication: Proceedings of the ASME Turbo Expo