To the Problem of Optimal Thermal Protection of Surfaces in Supersonic Flows
- 作者: Garaev K.1, Mukhametzyanov I.2
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隶属关系:
- Tupolev Kazan National Research Technical University
- Chistopol Branch “Vostok”
- 期: 卷 62, 编号 1 (2019)
- 页面: 52-58
- 栏目: Aero- and Gas-Dynamics of Flight Vehicles and Their Engines
- URL: https://journals.rcsi.science/1068-7998/article/view/230826
- DOI: https://doi.org/10.3103/S1068799819010070
- ID: 230826
如何引用文章
详细
The optimization problem of heat and mass transfer in the boundary layer on permeable profiles in supersonic gas flows is considered. Unlike the previous works of this direction, the analytical formula for optimal gas flow through the permeable surface is obtained in the present work, it is more convenient for application in engineering practice. The results of computing experiment are given.
作者简介
K. Garaev
Tupolev Kazan National Research Technical University
Email: m.ilshat@mail.ru
俄罗斯联邦, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
I. Mukhametzyanov
Chistopol Branch “Vostok”
编辑信件的主要联系方式.
Email: m.ilshat@mail.ru
俄罗斯联邦, ul. Engel’sa 127a, Chistopol, Tatarstan, 422981