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A Study on the Flight Performance of a Canard-Configuration WIG in a Seaway

A Study on the Flight Performance of a Canard-Configuration WIG in a Seaway
鸭式布局地效翼机航道飞行性能研究
批准号:
23360385
负责人:
HIDETSUGU Iwashita
金额:
$11.73万
依托单位:
依托单位国家:
日本
项目类别:
Grant-in-Aid for Scientific Research (B)
财政年份:
2011
资助国家:
日本
项目状态:
已结题
起止时间:
2011-04-01 至 2014-03-31

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中文摘要
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英文摘要
WIG (Wing In Ground effect) is an unconventional airplane and/or ship which enables the high-speed and mass sea-transportation in the future utilizing the high lift-to-drag ratio of the wing flying near the sea surface. In this study, the aerodynamic properties of the WIG are investigated from the theoretical and experimental points of view. A canard-configuration WIG which can improve the seakeeping performance in a seaway is proposed and made clear its aerodynamic properties. The theoretical calculation method and the experimental method in the wind tunnel and in the towing tank are also established through the study.
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