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An experimental study of subcritical transition into thermoacoustic oscillations in a swirl stabilized model gas turbine combustor (2020)

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