Email this article To the Problem of Optimal Thermal Protection of Surfaces in Supersonic Flows
- Authors: Garaev K.G.1, Mukhametzyanov I.R.2
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Affiliations:
- Tupolev Kazan National Research Technical University
- Chistopol Branch “Vostok”
- Issue: Vol 62, No 1 (2019)
- Pages: 52-58
- Section: 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
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Abstract
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.
About the authors
K. G. Garaev
Tupolev Kazan National Research Technical University
Email: m.ilshat@mail.ru
Russian Federation, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
I. R. Mukhametzyanov
Chistopol Branch “Vostok”
Author for correspondence.
Email: m.ilshat@mail.ru
Russian Federation, ul. Engel’sa 127a, Chistopol, Tatarstan, 422981
