Study of flame stabilization in a model gas turbine combustor
- 作者: Mingazov B.G.1, Baklanov A.V.1
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隶属关系:
- Tupolev Kazan National Research Technical University
- 期: 卷 59, 编号 3 (2016)
- 页面: 408-413
- 栏目: 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
如何引用文章
详细
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.
作者简介
B. Mingazov
Tupolev Kazan National Research Technical University
Email: andreybaklanov@bk.ru
俄罗斯联邦, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
A. Baklanov
Tupolev Kazan National Research Technical University
编辑信件的主要联系方式.
Email: andreybaklanov@bk.ru
俄罗斯联邦, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
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