Investigation of Mixing Enhancement Mechanism Caused by Pseudo-Shock Wave
Project/Area Number |
20360081
|
Research Category |
Grant-in-Aid for Scientific Research (B)
|
Allocation Type | Single-year Grants |
Section | 一般 |
Research Field |
Fluid engineering
|
Research Institution | Tohoku University |
Principal Investigator |
MASUYA Goro 東北大学, 大学院・工学研究科, 教授 (20271869)
|
Co-Investigator(Kenkyū-buntansha) |
TAKITA Kenichi 東北大学, 大学院・工学研究科, 准教授 (80282101)
KOUCHI Toshinori 東北大学, 大学院・工学研究科, 助教 (40415922)
|
Project Period (FY) |
2008 – 2011
|
Project Status |
Completed (Fiscal Year 2011)
|
Budget Amount *help |
¥19,890,000 (Direct Cost: ¥15,300,000、Indirect Cost: ¥4,590,000)
Fiscal Year 2011: ¥2,470,000 (Direct Cost: ¥1,900,000、Indirect Cost: ¥570,000)
Fiscal Year 2010: ¥2,340,000 (Direct Cost: ¥1,800,000、Indirect Cost: ¥540,000)
Fiscal Year 2009: ¥2,600,000 (Direct Cost: ¥2,000,000、Indirect Cost: ¥600,000)
Fiscal Year 2008: ¥12,480,000 (Direct Cost: ¥9,600,000、Indirect Cost: ¥2,880,000)
|
Keywords | 圧縮・非圧縮流 / 擬似衝撃波 / 乱流混合 / レーザー計測 / Large Eddy Simulation / 燃料噴射 |
Research Abstract |
Mixing of fuel injected into supersonic internal flow with a pseudo-shock wave, which appears in the combustor of a dual-mode ramjet engine, is significantly and non-isotropically improved. In order to clarify the mechanism of this mixing enhancement, injectant concentration and velocity distributions were measured using a particle image velocimetry (PIV)and a planar laser-induced fluorescence (PLIF), respectively. In addition, numerical simulations were carried out to understand the flowfield. As a result, we found that the pseudo-shock wave produced strong turbulence near the wall and it enhanced mixing of the jet.
|
Report
(6 results)
Research Products
(67 results)