Experimental Investigation of In-Hole Evolutionary Flow Behavior in a 777-Shaped Jet in Crossflow Via Refractive Index Matching-Based TR-PIV TechniqueSource: Journal of Turbomachinery:;2026:;volume( 148 ):;issue:001::page 1119Author:Huang, Weichen
,
Xu, Zhihan
,
Vicano, Valerio
,
Qu, Wenhai
,
Xiong, Jinbiao
,
Zhou, Wenwu
,
Liu, Yingzheng
DOI: 10.1115/1.4069421Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Abstract. The 777-shaped jet in crossflow (JICF) has been widely used in film cooling applications. To elucidate in-hole flow behavior and its evolution, time-resolved particle image velocimetry and refractive index matching were used to experimentally investigate the in-hole flow characteristics of the 777-shaped hole (35 deg of inclination angle) at velocity ratios (VRs) of 0.4, 0.8, and 1.2, with a density ratio of 1.0. Two in-hole low-speed zones were identified: at the trailing edge of the cylindrical section and within the diffuser. The region near the cylindrical section low-speed zone exhibited intensified vorticity, turbulent kinetic energy, and turbulent dissipation rate, attributed to clustered vortex shedding near the hole inlet. The complex formation of in-hole vorticity was further examined via spectral proper orthogonal decomposition. At VR ≤ 0.8, only a single Kelvin–Helmholtz (K–H) structure was observed at the trailing edge of the hole inlet. To verify the analysis at high VRs, an additional case (VR = 2.0) was considered. At VR ≥ 1.2, three K–H structures with negative vorticity were identified: at the trailing edge of the hole inlet, at the beginning of the diffuser, and within the in-hole region beneath the leading edge of the orifice. Overall, the findings of this study can enhance the experimental reference database on the in-hole flow characteristics of the 777-shaped hole and inform the design of shaped JICF structures for film cooling in gas turbines.
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| contributor author | Huang, Weichen | |
| contributor author | Xu, Zhihan | |
| contributor author | Vicano, Valerio | |
| contributor author | Qu, Wenhai | |
| contributor author | Xiong, Jinbiao | |
| contributor author | Zhou, Wenwu | |
| contributor author | Liu, Yingzheng | |
| date accessioned | 2026-08-23T08:34:50Z | |
| date available | 2026-08-23T08:34:50Z | |
| date copyright | 2026/01/01 | |
| date issued | 2026 | |
| identifier issn | 0889-504X | |
| identifier other | turbo-25-1028.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl1/handle/yetl/4316762 | |
| description abstract | Abstract. The 777-shaped jet in crossflow (JICF) has been widely used in film cooling applications. To elucidate in-hole flow behavior and its evolution, time-resolved particle image velocimetry and refractive index matching were used to experimentally investigate the in-hole flow characteristics of the 777-shaped hole (35 deg of inclination angle) at velocity ratios (VRs) of 0.4, 0.8, and 1.2, with a density ratio of 1.0. Two in-hole low-speed zones were identified: at the trailing edge of the cylindrical section and within the diffuser. The region near the cylindrical section low-speed zone exhibited intensified vorticity, turbulent kinetic energy, and turbulent dissipation rate, attributed to clustered vortex shedding near the hole inlet. The complex formation of in-hole vorticity was further examined via spectral proper orthogonal decomposition. At VR ≤ 0.8, only a single Kelvin–Helmholtz (K–H) structure was observed at the trailing edge of the hole inlet. To verify the analysis at high VRs, an additional case (VR = 2.0) was considered. At VR ≥ 1.2, three K–H structures with negative vorticity were identified: at the trailing edge of the hole inlet, at the beginning of the diffuser, and within the in-hole region beneath the leading edge of the orifice. Overall, the findings of this study can enhance the experimental reference database on the in-hole flow characteristics of the 777-shaped hole and inform the design of shaped JICF structures for film cooling in gas turbines. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Experimental Investigation of In-Hole Evolutionary Flow Behavior in a 777-Shaped Jet in Crossflow Via Refractive Index Matching-Based TR-PIV Technique | |
| type | Journal Paper | |
| journal volume | 148 | |
| journal issue | 1 | |
| journal title | Journal of Turbomachinery | |
| identifier doi | 10.1115/1.4069421 | |
| journal fristpage | 1119 | |
| journal lastpage | 1136 | |
| page | 18 | |
| tree | Journal of Turbomachinery:;2026:;volume( 148 ):;issue:001 | |
| contenttype | Fulltext |