Автор туралы ақпарат
Gorelov, Yu. G.
| Шығарылым | Бөлім | Атауы | Файл |
| Том 61, № 1 (2018) | Aircraft and Rocket Engine Design and Development | The 3D Computational Investigation of Film Cooling Effectiveness for Turbine Nozzle Vanes with “Meridian Constriction” and Shaped Film-Cooling Holes | |
| Том 61, № 3 (2018) | Aircraft and Rocket Engine Theory | 3D Investigations of the High Pressure Turbine Vane Platform Convection Cooling and Convection-Film Cooling | |
| Том 62, № 1 (2019) | Aircraft and Rocket Engine Theory | Verification of the Film Cooling Calculations for Nozzle Vane Leading Edges in ANSYS CFX | |
| Том 62, № 3 (2019) | Aircraft and Rocket Engine Theory | 3D Investigation of Film Cooling Effectiveness for Nozzle Vane Platform of High Pressure Turbine with “Meridian Constriction” and Laidback Fan-Shaped Film-Cooling Holes |