The 3D Computational Investigation of Film Cooling Effectiveness for Turbine Nozzle Vanes with “Meridian Constriction” and Shaped Film-Cooling Holes |
| |
| Authors: | Yu G Gorelov K V Tyul’kov |
| |
| Institution: | 1.Salyut Gas Turbine Engineering Research and Production Centre,Moscow,Russia |
| |
| Abstract: | Active influence dimension of film cooling along the blade profile is investigated with using the Spalart–Allmaras turbulence model. The cooling effectiveness of vane platforms and vane fillets is studied with the use of perforation holes on the leading edge. |
| |
| Keywords: | |
| 本文献已被 SpringerLink 等数据库收录！ |
