Influence of the burner form on the combustion chamber outlet temperature field ripple for different modes of operation of gas turbine engines

This article describes a method of identifying combustion chamber temperature field ripple by the preparation of the set of nozzles in the engine. It shows combustion chamber temperature field ripple with a divergent nozzle and a convergent one used in the burner. The design of the combustion chambe...

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Bibliographic Details
Main Authors: A. N. Markushin, A. V. Baklanov
Format: Article
Language:English
Published: Samara National Research University 2016-12-01
Series:Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение
Subjects:
Online Access:https://journals.ssau.ru/vestnik/article/viewFile/3113/3025