Behavior of Titanium Alloys in Aerodynamic Heating of Hypersonic Airplanes

V. A. Afanas’ev; P. V. Nikitin; O. V. Tushavina

doi:10.3103/S1068798X1901012X

Behavior of Titanium Alloys in Aerodynamic Heating of Hypersonic Airplanes

作者: Afanas’ev V.A.¹, Nikitin P.V.¹, Tushavina O.V.¹
隶属关系:
1. Moscow Aviation Institute
期: 卷 39, 编号 1 (2019)
页面: 25-30
栏目: Article
URL: https://journals.rcsi.science/1068-798X/article/view/227619
DOI: https://doi.org/10.3103/S1068798X1901012X
ID: 227619

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详细

The requirements on the use of titanium alloys used as thermal protection in hypersonic airplanes are considered. The ignition of titanium alloys in aerodynamic heating is analyzed. A mathematical model is proposed for the surface oxidation of the alloys in a high-temperature air flux.