作者的详细信息

Шевченко, Юлия Николаевна

期	栏目	标题	文件
卷 15, 编号 4 (2014)	Articles	Comparison of direct and reverse cycle of the thermal control system for the non-hermetic spacecrafts	(Rus)
卷 24, 编号 1 (2023)	Section 2. Aviation and Space Technology	Design of a thermal control system with a two-phase coolant for a spacecraft with a capacity of 7 kW	(Rus)
卷 21, 编号 3 (2020)	Section 2. Aviation and Space Technology	Flow dynamics in the radial-annular cavity of turbomachines	(Eng)
卷 20, 编号 3 (2019)	Section 2. Aviation and Space Technology	Determining thermal resistance in the model of the liquid circuit of spacecraft thermal control system	(Eng)
卷 20, 编号 3 (2019)	Section 2. Aviation and Space Technology	Calculation of complex heat transfer in the liquid circuit of the spacecraft thermal control system based on real topology and thermophysical properties	(Eng)
卷 25, 编号 1 (2024)	Section 2. Aviation and Space Technology	Power engineering of the tangential supply device of the microturbine of the thermal control system of a promising spacecraft	(Rus) (Eng)