Автор туралы ақпарат
Yaroslavtsev, N. L.
| Шығарылым | Бөлім | Атауы | Файл |
| Том 59, № 1 (2016) | Aircraft and Rocket Engine Design and Development | Development of the design scheme of cooling for a nozzle vane of high pressure turbine of gas turbine engine | |
| Том 59, № 3 (2016) | Aircraft and Rocket Engine Design and Development | Diagnostics of efficiency for a cooling system of compact heat exchangers with coplanar channels |