Author Details
Шевченко, Юлия Николаевна
Issue | Section | Title | File |
Vol 15, No 4 (2014) | Articles | Comparison of direct and reverse cycle of the thermal control system for the non-hermetic spacecrafts |
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Vol 24, No 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 |
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Vol 21, No 3 (2020) | Section 2. Aviation and Space Technology | Flow dynamics in the radial-annular cavity of turbomachines |
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Vol 20, No 3 (2019) | Section 2. Aviation and Space Technology | Determining thermal resistance in the model of the liquid circuit of spacecraft thermal control system |
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Vol 20, No 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 |
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