Thermodynamic study of the characteristics of small-size centrifugal compressor turbojet disk gtj using solidworks cad package, and mathematical modeling of cosmos

Аuthors

Lapushkin V. N., Novikov A. V.^*, Rodchenko V. V.^**

Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia

*e-mail: novikov@brainse.ru
**e-mail: dekanat6@cosmos.com.ru

Abstract

Article deals with the possibility of using modem computer technology in the design of small gas turbine disk motor-generators for the analysis of thermodynamic processes on the highway the engine in a small amount, in the example simulation of a centrifugal compressor.

Keywords:

mathematical modeling, centrifugal compressor, automated design