2013 Fiscal Year Final Research Report
Fundamental study on the innovative film cooling technologies to suppress the mixing process with adding swirling motion to the coolant
Project/Area Number |
23560229
|
Research Category |
Grant-in-Aid for Scientific Research (C)
|
Allocation Type | Multi-year Fund |
Section | 一般 |
Research Field |
Thermal engineering
|
Research Institution | Osaka University |
Principal Investigator |
|
Co-Investigator(Kenkyū-buntansha) |
KOMIYAMA Masaharu 大阪大学, 大学院工学研究科, 准教授 (40178372)
|
Co-Investigator(Renkei-kenkyūsha) |
ODA Yutaka 大阪大学, 大学院工学研究科, 講師 (50403150)
|
Project Period (FY) |
2011 – 2013
|
Keywords | 物質伝達 / 熱伝達 / フィルム冷却 / 旋回流 / 感圧塗料 / レーザ誘起蛍光法 / PIV / ガスタービン |
Research Abstract |
This study has been conducted to investigate a new film cooling method that utilizes swirling coolant flow through circular and shaped film cooling holes. The mixing phenomena with a film cooling air and a mainstream was measured by a instantaneous and simultaneous LIF and PIV methods, and the film cooling effectiveness on the wall was measured by PSP. It appeared from the results that, in the case of a circular film-cooling hole, the penetration of the coolant jet into the mainstream was suppressed by the strong swirling motion of the coolant and attained 100% heigher film cooling effectiveness. As a result, the film cooling effectiveness on the wall maintained a higher value behind the cooling hole over a long range. Additionally, the kidney vortex structure disappeared. For the shaped film cooling hole, the coolant jet spreads wider in the span-wise direction. Thus, the pitch-averaged film cooling effectiveness downstream was 50% higher than that in the non-swirling case.
|
-
-
-
-
-
-
-
-
-
-
-
[Presentation] Aerothermal Investigations on Mixing Flow Field of Film Cooling with Swirling Coolant Flow2011
Author(s)
Takeishi, K., Komiyama, M., Oda, Y., Egawa, Y., and Kitamura, T.
Organizer
ASME Turbo Expo 2011
Place of Presentation
Vancouver, Canada
Year and Date
20110000
-
-
-
-
-