Parametric identification of a mathematical model of heat transfer in carbon–carbon (C–C) materials for aeronautical application

Author:

Alifanov O. M.,Budnik S. A.,Nenarokomov A. V.,Titov D. M.

Publisher

Allerton Press

Subject

Aerospace Engineering

Reference7 articles.

1. Kuznetsova, E.L. and Kolesnik, S.A., Simulation of Heat and Mass Transfer in Composite Heat Protective Materials under High Temperature Conditions, Izv.Vuz. Av. Tekhnika, 2012, vol. 55, no. 1, pp. 31–35 [Russian Aeronautics (Engl. Transl.), vol. 55, no. 1, pp. 41–49].

2. Wang, Z.J., Hong, Ye, and Kretov, A.S., Calculation of Heat Conduction in Aerospace Plane Thermal Protection System, Izv.Vuz. Av. Tekhnika, 2013, vol. 56, no. 3, pp. 3–6 [Russian Aeronautics (Engl. Transl.), vol. 56, no. 3, pp. 3–6].

3. Albano, M., Micheli, D., Gradoni, G., Morles, R.B., et al., Electromagnetic Shielding of Thermal Protection System for Hypersonic Vehicles, Acta Astronautica, 2013, vol. 87, pp. 30–39.

4. Albano, M., Nenarokomov, A.V., Delhi, A., and Marchetti, M., Properties of Carbon and SiC Foam as Thermal Insulator for Space Thermal Protection Systems, Proc. of the 66th Int. Astronautical Congress, Jerusalem, Israel, At IAC-15-C2.4.

5. Muzylev, N.V., On the Uniqueness of the Simultaneous Determination of Thermal Conductivity and Volume Heat Capacity, Zh. Vychisl. Mat. Mat. Fiz., vol. 23, no. 1, pp. 102–108 [USSR Comput. Math. and Math. Phys. (Engl. Transl.), vol. 23, no. 1, pp. 69–73.

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