{"title":"2d桅杆/帆几何形状上的静压分布","authors":"S. Wilkinson","doi":"10.5957/MT1.1989.26.4.333","DOIUrl":null,"url":null,"abstract":"A variable-camber airfoil with integral pressure tappings has been built to investigate the nature of the flows around two-dimensional, highly cambered, sail-like airfoil sections with circular masts. Data have been obtained in the form of static pressure distributions over representative ranges of Reynolds number, camber ratio, incidence angle, mast diameter/chord ratio and mast angle. Two sail shapes--based on the NACA a = 0.8 and NACA 63 mean-line camber distributions--were involved in the test program. All flow regimes present have been identified and related to the salient model and flow parameters.","PeriodicalId":49310,"journal":{"name":"Marine Technology and Sname News","volume":"362 1","pages":"333-337"},"PeriodicalIF":0.0000,"publicationDate":"1989-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"21","resultStr":"{\"title\":\"STATIC PRESSURE DISTRIBUTIONS OVER 2D MAST/SAIL GEOMETRIES\",\"authors\":\"S. Wilkinson\",\"doi\":\"10.5957/MT1.1989.26.4.333\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"A variable-camber airfoil with integral pressure tappings has been built to investigate the nature of the flows around two-dimensional, highly cambered, sail-like airfoil sections with circular masts. Data have been obtained in the form of static pressure distributions over representative ranges of Reynolds number, camber ratio, incidence angle, mast diameter/chord ratio and mast angle. Two sail shapes--based on the NACA a = 0.8 and NACA 63 mean-line camber distributions--were involved in the test program. All flow regimes present have been identified and related to the salient model and flow parameters.\",\"PeriodicalId\":49310,\"journal\":{\"name\":\"Marine Technology and Sname News\",\"volume\":\"362 1\",\"pages\":\"333-337\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"1989-10-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"21\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Marine Technology and Sname News\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.5957/MT1.1989.26.4.333\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q4\",\"JCRName\":\"Engineering\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Marine Technology and Sname News","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.5957/MT1.1989.26.4.333","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q4","JCRName":"Engineering","Score":null,"Total":0}
引用次数: 21
摘要
一个可变弧度翼型与整体压力抽头已建成调查流动的性质周围二维,高度弧度,帆状翼型部分与圆形桅杆。数据以雷诺数、弧度比、入射角、桅杆直径/弦比和桅杆角的代表性范围内的静压分布的形式获得。两种船帆形状——基于NACA a = 0.8和NACA 63平均值曲线分布——参与了测试程序。所有的流动形式都已确定,并与显著模型和流动参数相关。
STATIC PRESSURE DISTRIBUTIONS OVER 2D MAST/SAIL GEOMETRIES
A variable-camber airfoil with integral pressure tappings has been built to investigate the nature of the flows around two-dimensional, highly cambered, sail-like airfoil sections with circular masts. Data have been obtained in the form of static pressure distributions over representative ranges of Reynolds number, camber ratio, incidence angle, mast diameter/chord ratio and mast angle. Two sail shapes--based on the NACA a = 0.8 and NACA 63 mean-line camber distributions--were involved in the test program. All flow regimes present have been identified and related to the salient model and flow parameters.
期刊介绍:
The Marine Technology Society Journal is the flagship publication of the Marine Technology Society. It publishes the highest caliber, peer-reviewed papers, six times a year, on subjects of interest to the society: marine technology, ocean science, marine policy, and education.