Shouzuo Li, Xiangyu Wang, Yishu Liu, Songtao Wang, Le Cai
{"title":"采用内横流供给结构的双射流气膜冷却的气动传热性能","authors":"Shouzuo Li, Xiangyu Wang, Yishu Liu, Songtao Wang, Le Cai","doi":"10.1016/j.ijthermalsci.2025.110321","DOIUrl":null,"url":null,"abstract":"<div><div>The double-jet film-cooling structure is recognized as an effective method for cooling the hot-section parts of turbines. Recent studies highlight the significant impact of internal supply configurations on the aerodynamic and thermal characteristics of external film cooling. Therefore, this study investigates the aerodynamic and heat transfer performance of double-jet film-cooling holes under crossflow conditions, both with and without ribs, through numerical simulation. The study examines both positive and negative crossflow supply directions across four blowing ratios (ranging from M = 0.5 to 2.0), using a cavity supply case as the baseline for comparison. By modifying the geometric and aerodynamic boundary conditions, the focus is on analyzing the changes in the flow field structure, aerodynamic losses, and cooling performance across various supply configurations. The results reveal that at low blowing ratios, double-jet film-cooling holes are significantly affected by crossflow. Compared to the cavity supply case, the discharge coefficient in the crossflow cases decreases by up to 45.1 %. Different internal crossflow supply configurations exhibit distinct optimal blowing ratios, with the smooth crossflow supply configurations beginning to demonstrate advantages in cooling performance when M ≥ 2.0. This research emphasizes the importance of a rational configuration of the cooling structure—including the internal structure, supply direction, and hole parameters—for substantially enhancing film cooling performance under high blowing ratios (M ≥ 1.5). The findings deliver actionable design principles and performance optimization guidelines for double-jet film cooling configurations.</div></div>","PeriodicalId":341,"journal":{"name":"International Journal of Thermal Sciences","volume":"220 ","pages":"Article 110321"},"PeriodicalIF":5.0000,"publicationDate":"2025-09-23","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Aerodynamic and heat transfer performance of double-jet film cooling using internal crossflow supply configuration\",\"authors\":\"Shouzuo Li, Xiangyu Wang, Yishu Liu, Songtao Wang, Le Cai\",\"doi\":\"10.1016/j.ijthermalsci.2025.110321\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<div><div>The double-jet film-cooling structure is recognized as an effective method for cooling the hot-section parts of turbines. Recent studies highlight the significant impact of internal supply configurations on the aerodynamic and thermal characteristics of external film cooling. Therefore, this study investigates the aerodynamic and heat transfer performance of double-jet film-cooling holes under crossflow conditions, both with and without ribs, through numerical simulation. The study examines both positive and negative crossflow supply directions across four blowing ratios (ranging from M = 0.5 to 2.0), using a cavity supply case as the baseline for comparison. By modifying the geometric and aerodynamic boundary conditions, the focus is on analyzing the changes in the flow field structure, aerodynamic losses, and cooling performance across various supply configurations. The results reveal that at low blowing ratios, double-jet film-cooling holes are significantly affected by crossflow. Compared to the cavity supply case, the discharge coefficient in the crossflow cases decreases by up to 45.1 %. Different internal crossflow supply configurations exhibit distinct optimal blowing ratios, with the smooth crossflow supply configurations beginning to demonstrate advantages in cooling performance when M ≥ 2.0. This research emphasizes the importance of a rational configuration of the cooling structure—including the internal structure, supply direction, and hole parameters—for substantially enhancing film cooling performance under high blowing ratios (M ≥ 1.5). The findings deliver actionable design principles and performance optimization guidelines for double-jet film cooling configurations.</div></div>\",\"PeriodicalId\":341,\"journal\":{\"name\":\"International Journal of Thermal Sciences\",\"volume\":\"220 \",\"pages\":\"Article 110321\"},\"PeriodicalIF\":5.0000,\"publicationDate\":\"2025-09-23\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"International Journal of Thermal Sciences\",\"FirstCategoryId\":\"5\",\"ListUrlMain\":\"https://www.sciencedirect.com/science/article/pii/S1290072925006441\",\"RegionNum\":2,\"RegionCategory\":\"工程技术\",\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q1\",\"JCRName\":\"ENGINEERING, MECHANICAL\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"International Journal of Thermal Sciences","FirstCategoryId":"5","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S1290072925006441","RegionNum":2,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q1","JCRName":"ENGINEERING, MECHANICAL","Score":null,"Total":0}
Aerodynamic and heat transfer performance of double-jet film cooling using internal crossflow supply configuration
The double-jet film-cooling structure is recognized as an effective method for cooling the hot-section parts of turbines. Recent studies highlight the significant impact of internal supply configurations on the aerodynamic and thermal characteristics of external film cooling. Therefore, this study investigates the aerodynamic and heat transfer performance of double-jet film-cooling holes under crossflow conditions, both with and without ribs, through numerical simulation. The study examines both positive and negative crossflow supply directions across four blowing ratios (ranging from M = 0.5 to 2.0), using a cavity supply case as the baseline for comparison. By modifying the geometric and aerodynamic boundary conditions, the focus is on analyzing the changes in the flow field structure, aerodynamic losses, and cooling performance across various supply configurations. The results reveal that at low blowing ratios, double-jet film-cooling holes are significantly affected by crossflow. Compared to the cavity supply case, the discharge coefficient in the crossflow cases decreases by up to 45.1 %. Different internal crossflow supply configurations exhibit distinct optimal blowing ratios, with the smooth crossflow supply configurations beginning to demonstrate advantages in cooling performance when M ≥ 2.0. This research emphasizes the importance of a rational configuration of the cooling structure—including the internal structure, supply direction, and hole parameters—for substantially enhancing film cooling performance under high blowing ratios (M ≥ 1.5). The findings deliver actionable design principles and performance optimization guidelines for double-jet film cooling configurations.
期刊介绍:
The International Journal of Thermal Sciences is a journal devoted to the publication of fundamental studies on the physics of transfer processes in general, with an emphasis on thermal aspects and also applied research on various processes, energy systems and the environment. Articles are published in English and French, and are subject to peer review.
The fundamental subjects considered within the scope of the journal are:
* Heat and relevant mass transfer at all scales (nano, micro and macro) and in all types of material (heterogeneous, composites, biological,...) and fluid flow
* Forced, natural or mixed convection in reactive or non-reactive media
* Single or multi–phase fluid flow with or without phase change
* Near–and far–field radiative heat transfer
* Combined modes of heat transfer in complex systems (for example, plasmas, biological, geological,...)
* Multiscale modelling
The applied research topics include:
* Heat exchangers, heat pipes, cooling processes
* Transport phenomena taking place in industrial processes (chemical, food and agricultural, metallurgical, space and aeronautical, automobile industries)
* Nano–and micro–technology for energy, space, biosystems and devices
* Heat transport analysis in advanced systems
* Impact of energy–related processes on environment, and emerging energy systems
The study of thermophysical properties of materials and fluids, thermal measurement techniques, inverse methods, and the developments of experimental methods are within the scope of the International Journal of Thermal Sciences which also covers the modelling, and numerical methods applied to thermal transfer.