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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)

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