New Approach to Preventing External Overheating of High-Speed Aircraft

被引：0

作者：

Formalev V.F. ^{[1
]}

Kolesnik S.A. ^{[1
]}

Garibyan B.A. ^{[1
]}

Pashkov O.A. ^{[1
]}

Pegachkova E.A. ^{[1
]}

机构：

[1] Moscow Aviation Institute, Moscow

来源：

Russian Engineering Research | 2024年 / 44卷 / 5期

基金：

俄罗斯科学基金会;

关键词：

aerodynamic heating; anisotropy; complex heat transfer; composites; heat conduction; heat fluxes; high-speed aircraft; hydrodynamic flow; near-wall flow; overheating; surface temperature; thermal conductivity tensor; thermal protection; viscous gas dynamics;

D O I：

10.3103/S1068798X24700904

中图分类号：

学科分类号：

摘要：

Abstract: External overheating of high-speed aircraft may be prevented by means of composites with significant longitudinal anisotropy. (The longitudinal thermal conductivity is two orders of magnitude greater than the transverse thermal conductivity.) In this approach, the heat fluxes that result from aerodynamic heating are channeled within the anisotropic composites from the hottest region (the front critical point) to the tail of the truncated cone. As a result, the vicinity of the front critical point is cooled and the tail of the cone is heated, with considerable decrease in the associated heat fluxes. © Allerton Press, Inc. 2024. ISSN 1068-798X, Russian Engineering Research, 2024, Vol. 44, No. 5, pp. 705–708. Allerton Press, Inc., 2024. Russian Text The Author(s), 2024, published in STIN, 2024, No. 4, pp. 13–16.

引用

页码：705 / 708

页数：3

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