Study of flame stabilization in a model gas turbine combustor
- Авторлар: Mingazov B.G.1, Baklanov A.V.1
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Мекемелер:
- Tupolev Kazan National Research Technical University
- Шығарылым: Том 59, № 3 (2016)
- Беттер: 408-413
- Бөлім: Aircraft and Rocket Engine Design and Development
- URL: https://journals.rcsi.science/1068-7998/article/view/229804
- DOI: https://doi.org/10.3103/S1068799816030181
- ID: 229804
Дәйексөз келтіру
Аннотация
The paper reports the results of experimental studies and numerical calculations of the flame stabilization process in the model gas turbine combustor. The mathematical model of the process in the combustor is presented. Using this model, the main parameters of combustors with different ratios of total area of the holes in the combustion zone to total area of all holes, are determined.
Негізгі сөздер
Авторлар туралы
B. Mingazov
Tupolev Kazan National Research Technical University
Email: andreybaklanov@bk.ru
Ресей, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
A. Baklanov
Tupolev Kazan National Research Technical University
Хат алмасуға жауапты Автор.
Email: andreybaklanov@bk.ru
Ресей, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
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