Experimental studies on the development of finite-wing wake

碩士 === 國立成功大學 === 航空太空工程學系 === 90 === The characteristics of the wake development of a finite wing under 3 different angles of attack were studied through experimental means. X-type hotwire anemometer was utilized to measure both the velocity of x and y direction of the three-dimensional...

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Bibliographic Details
Main Author: 鄭照仁
Other Authors: F. B. Hsiao
Format: Others
Language:zh-TW
Published: 2002
Online Access:http://ndltd.ncl.edu.tw/handle/70702648529893404894

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