Conceptual Protection Model for Especially Heat-Proof Materials in Hypersonic Oxidizing Gas Flows

Author:

Terentieva V. S.,Astapov A. N.

Publisher

Allerton Press

Subject

Metals and Alloys,Surfaces, Coatings and Films,Mechanics of Materials

Reference33 articles.

1. Astapov, A.N. and Terentieva, V.S., Analysis of hypersonic systems design practice and its thermal conditions securing (a survey), Tepl. Prots. Tekh., 2014, vol. 6, no. 1, pp. 2–11.

2. Astapov, A.N. and Terentieva, V.S., Review of domestic developments in the field of protection of carbon-containing materials against gas corrosion and erosion in high-speed plasma flows, Izv. Vyssh. Uchebn. Zaved. Poroshk. Metall. Funkts. Pokryt., 2014, no. 4, pp. 50–70. doi 10.1707/1997-308X-2014-4-50-70

3. Molev, G.V. and Mirzabekyants, N.S., Methods for improving the resistance to oxidation of carbon materials in air at elevated temperatures, Khim. Tverd. Topl., 1998, no. 1, pp. 89–100.

4. Opeka, M.M., Talmy, I.G., and Zaykoski, J.A., Oxidation-based materials selection for 2000 C + hypersonic aerosurfaces: Theoretical consideration and historical experience, J. Mater. Sci., 2004, vol. 39, no. 19, pp. 5887–5904. doi 10.1023/B:JMSC.0000041686.21788.77

5. Ohlhorst, C.W., Vaughn, W.L., Lewis, R.K., and Milhoan, J.D., Arc jet results on candidate high temperature coatings for NASA’s NGLT refractory composite leading edge task, in Proc. APS-II-77, JANNAF 27th Airbreathing Propulsion Meeting, Colorado Springs, CO: 2003.

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