E. Martínez-Sandoval, Dulce Graciano, Fernando Zenaido SIERRA Espinosa, J García Castrejón
{"title":"Enhanced film cooling effectiveness by wall-roughness in cooling hole of turbine blade","authors":"E. Martínez-Sandoval, Dulce Graciano, Fernando Zenaido SIERRA Espinosa, J García Castrejón","doi":"10.1615/jenhheattransf.2023049163","DOIUrl":null,"url":null,"abstract":"The film cooling is investigated numerically for gas turbine blade cooling. Film cooling performance is vital for blade safe operation. By calculating the film cooling effectiveness, the wall roughness inside the cooling hole effect is evaluated. Wall roughness by a turbulence promoter of aspect ratio K = L/h from 6 to 14, varying the pitch L and keeping constant the height h. Blowing ratio range from M = 0.5 to 2 and fixed mainstream Reynolds number, Re = 2.0 x 105 are tested. The cooling hole and flat plate surface with angle of 35o is used to compare the results and validate the CFD approach assessing the turbulence models k-ε RNG and RSM. A swirl flow develops inside the cooling hole due to installing the turbulence promoter. The coolant discharge turbulence parameters modify the normal case. The momentum and heat transfer rates have an impact on the film cooling performance. The results indicate film cooling effectiveness and surface protection enhancement of 9.84%, and 19.4%, respectively, for the best aspect ratio and blowing ratio. The coolant roughness may be used to improve the design of coolant hole and to reduce the number of orifices needed for safe gas turbine blades.","PeriodicalId":50208,"journal":{"name":"Journal of Enhanced Heat Transfer","volume":"38 1","pages":""},"PeriodicalIF":1.5000,"publicationDate":"2023-12-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Journal of Enhanced Heat Transfer","FirstCategoryId":"5","ListUrlMain":"https://doi.org/10.1615/jenhheattransf.2023049163","RegionNum":4,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q3","JCRName":"ENGINEERING, MECHANICAL","Score":null,"Total":0}
引用次数: 0
Abstract
The film cooling is investigated numerically for gas turbine blade cooling. Film cooling performance is vital for blade safe operation. By calculating the film cooling effectiveness, the wall roughness inside the cooling hole effect is evaluated. Wall roughness by a turbulence promoter of aspect ratio K = L/h from 6 to 14, varying the pitch L and keeping constant the height h. Blowing ratio range from M = 0.5 to 2 and fixed mainstream Reynolds number, Re = 2.0 x 105 are tested. The cooling hole and flat plate surface with angle of 35o is used to compare the results and validate the CFD approach assessing the turbulence models k-ε RNG and RSM. A swirl flow develops inside the cooling hole due to installing the turbulence promoter. The coolant discharge turbulence parameters modify the normal case. The momentum and heat transfer rates have an impact on the film cooling performance. The results indicate film cooling effectiveness and surface protection enhancement of 9.84%, and 19.4%, respectively, for the best aspect ratio and blowing ratio. The coolant roughness may be used to improve the design of coolant hole and to reduce the number of orifices needed for safe gas turbine blades.
期刊介绍:
The Journal of Enhanced Heat Transfer will consider a wide range of scholarly papers related to the subject of "enhanced heat and mass transfer" in natural and forced convection of liquids and gases, boiling, condensation, radiative heat transfer.
Areas of interest include:
■Specially configured surface geometries, electric or magnetic fields, and fluid additives - all aimed at enhancing heat transfer rates. Papers may include theoretical modeling, experimental techniques, experimental data, and/or application of enhanced heat transfer technology.
■The general topic of "high performance" heat transfer concepts or systems is also encouraged.