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Abstract
In order to improve the lift capability of the wing-in-ground effect craft, the experimental aerodynamic performances were conducted for the ground effect wings through setting the vortex generators. Its performances have been evaluated the higher lift enhancement by controlling the stall at the higher angles of attack even if falling behind at the lower them.
Journal
- 年次大会講演論文集 : JSME annual meeting [List of Volumes]
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年次大会講演論文集 : JSME annual meeting 2005(2), 129-130, 2005-09-18 [Table of Contents]
The Japan Society of Mechanical Engineers