Guo-bing Huang (黄国兵), Han Hu (胡晗), Cai-huan Wang (王才欢), Lan Du (杜兰)
{"title":"Shock waves and water wing in slit-type energy dissipaters","authors":"Guo-bing Huang (黄国兵), Han Hu (胡晗), Cai-huan Wang (王才欢), Lan Du (杜兰)","doi":"10.1016/S1001-6058(16)60762-X","DOIUrl":null,"url":null,"abstract":"<div><p>The slit-type energy dissipater (STED) is widely used in hydraulic projects of high water head, large discharge, and narrow river valley, thanks to its simple structure and high efficiency. However, the water wing caused by the shock waves in the contraction section of the STED may bring about harmful effects. A coefficient is introduced for the application of Ippen's theory in the STED. The expression of the coefficient is experimentally obtained. Simplified formulas to calculate the shock wave angle and the water wing scope are theoretically derived, with relative errors within 5%.</p></div>","PeriodicalId":66131,"journal":{"name":"水动力学研究与进展:英文版","volume":"29 3","pages":"Pages 504-509"},"PeriodicalIF":3.4000,"publicationDate":"2017-06-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"https://sci-hub-pdf.com/10.1016/S1001-6058(16)60762-X","citationCount":"7","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"水动力学研究与进展:英文版","FirstCategoryId":"1087","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S100160581660762X","RegionNum":3,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q1","JCRName":"MECHANICS","Score":null,"Total":0}
引用次数: 7
Abstract
The slit-type energy dissipater (STED) is widely used in hydraulic projects of high water head, large discharge, and narrow river valley, thanks to its simple structure and high efficiency. However, the water wing caused by the shock waves in the contraction section of the STED may bring about harmful effects. A coefficient is introduced for the application of Ippen's theory in the STED. The expression of the coefficient is experimentally obtained. Simplified formulas to calculate the shock wave angle and the water wing scope are theoretically derived, with relative errors within 5%.