Yonghao Yu , Qionglei Hu , Kim Tiow Ooi , Qun Zheng , Mingcong Luo
{"title":"吸雨式压气机叶栅气动性能及流场特性研究","authors":"Yonghao Yu , Qionglei Hu , Kim Tiow Ooi , Qun Zheng , Mingcong Luo","doi":"10.1016/j.ast.2025.111030","DOIUrl":null,"url":null,"abstract":"<div><div>Rain ingestion significantly impacts axial compressor performance by modifying blade-surface water distribution and local aerodynamic loads. This study employs a linear-cascade two-phase flow test rig combined with high-speed imaging and a computer-vision algorithm to quantify rivulet and water-film dynamics under varying droplet sizes, water air ratio (WAR), cascade geometries, and attack angles. Results indicate that higher WAR and larger droplets increase total pressure loss, deviation-angle fluctuations, and early tendency of flow separation. Blade geometry amplifies these effects, with positive attack angle producing fewer but higher rivulets, and negative attack angle generating more numerous yet lower rivulets. Nonlinear correlations between rivulet height and local static pressure highlight the complex multiphase–aerodynamic interaction. These insights offer quantitative guidance for blade design and performance mitigation under wet-air conditions.</div></div>","PeriodicalId":50955,"journal":{"name":"Aerospace Science and Technology","volume":"168 ","pages":"Article 111030"},"PeriodicalIF":5.8000,"publicationDate":"2025-10-07","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Study on the aerodynamic performance and rivulet characteristics of a compressor cascade with rain ingestion\",\"authors\":\"Yonghao Yu , Qionglei Hu , Kim Tiow Ooi , Qun Zheng , Mingcong Luo\",\"doi\":\"10.1016/j.ast.2025.111030\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<div><div>Rain ingestion significantly impacts axial compressor performance by modifying blade-surface water distribution and local aerodynamic loads. This study employs a linear-cascade two-phase flow test rig combined with high-speed imaging and a computer-vision algorithm to quantify rivulet and water-film dynamics under varying droplet sizes, water air ratio (WAR), cascade geometries, and attack angles. Results indicate that higher WAR and larger droplets increase total pressure loss, deviation-angle fluctuations, and early tendency of flow separation. Blade geometry amplifies these effects, with positive attack angle producing fewer but higher rivulets, and negative attack angle generating more numerous yet lower rivulets. Nonlinear correlations between rivulet height and local static pressure highlight the complex multiphase–aerodynamic interaction. These insights offer quantitative guidance for blade design and performance mitigation under wet-air conditions.</div></div>\",\"PeriodicalId\":50955,\"journal\":{\"name\":\"Aerospace Science and Technology\",\"volume\":\"168 \",\"pages\":\"Article 111030\"},\"PeriodicalIF\":5.8000,\"publicationDate\":\"2025-10-07\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Aerospace Science and Technology\",\"FirstCategoryId\":\"5\",\"ListUrlMain\":\"https://www.sciencedirect.com/science/article/pii/S1270963825010934\",\"RegionNum\":1,\"RegionCategory\":\"工程技术\",\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q1\",\"JCRName\":\"ENGINEERING, AEROSPACE\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Aerospace Science and Technology","FirstCategoryId":"5","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S1270963825010934","RegionNum":1,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q1","JCRName":"ENGINEERING, AEROSPACE","Score":null,"Total":0}
Study on the aerodynamic performance and rivulet characteristics of a compressor cascade with rain ingestion
Rain ingestion significantly impacts axial compressor performance by modifying blade-surface water distribution and local aerodynamic loads. This study employs a linear-cascade two-phase flow test rig combined with high-speed imaging and a computer-vision algorithm to quantify rivulet and water-film dynamics under varying droplet sizes, water air ratio (WAR), cascade geometries, and attack angles. Results indicate that higher WAR and larger droplets increase total pressure loss, deviation-angle fluctuations, and early tendency of flow separation. Blade geometry amplifies these effects, with positive attack angle producing fewer but higher rivulets, and negative attack angle generating more numerous yet lower rivulets. Nonlinear correlations between rivulet height and local static pressure highlight the complex multiphase–aerodynamic interaction. These insights offer quantitative guidance for blade design and performance mitigation under wet-air conditions.
期刊介绍:
Aerospace Science and Technology publishes articles of outstanding scientific quality. Each article is reviewed by two referees. The journal welcomes papers from a wide range of countries. This journal publishes original papers, review articles and short communications related to all fields of aerospace research, fundamental and applied, potential applications of which are clearly related to:
• The design and the manufacture of aircraft, helicopters, missiles, launchers and satellites
• The control of their environment
• The study of various systems they are involved in, as supports or as targets.
Authors are invited to submit papers on new advances in the following topics to aerospace applications:
• Fluid dynamics
• Energetics and propulsion
• Materials and structures
• Flight mechanics
• Navigation, guidance and control
• Acoustics
• Optics
• Electromagnetism and radar
• Signal and image processing
• Information processing
• Data fusion
• Decision aid
• Human behaviour
• Robotics and intelligent systems
• Complex system engineering.
Etc.