Mathematical Modeling of Heat Transfer Processes in a Wall with a Regular Pseudo-pore Structure

Author:

Starikov P.,Ionov A.,Seliverstov S.,Borovik I.,Matushkin A.

Publisher

Springer Singapore

Reference8 articles.

1. Starikov, P. A. (2017). The gas turbine engine fuel system for a winged target. Bachelor Thesis, Moscow Aviation Institute.

2. Agapov, A. V., Bogdanov, V. N., Borovikov, D. A., Ionov, A. V., Seliverstov, S. D., & Starikov, P. A. (2016). Mathematical identification and design problems of small-size GTE. Scientific and Technical Herald of the Volga Region № 6, 120, 28–32.

3. Shishkin, D. A., & Zelenov, S. N. (2012). In R. E. Alekseeva (Ed.), Combustion chambers of gas turbine engines. Nizhny Novgorod: Nizhny Novgorod State Technical University.

4. Matushkin, A. A. (2012). Constructive improvement of the cooling system for working blades of high-temperature GTE turbines. Ph.D. Dissertation, Moscow Aviation Institute.

5. Matushkin, A. A., & Nesterenko, V. G. (2010). Constructive methods for improving the film cooling system for working blades of turbines of the VRD. Electronic Journal-Trudy MAI, 39.

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