发明名称 |
AIRFOIL SYSTEM FOR CRUISING FLIGHT |
摘要 |
<p>An airfoil system includes an airfoil body and at least one flexible strip. The airfoil body has a top surface and a bottom surface, a chord length, a span, and a maximum thickness. Each flexible strip is attached along at least one edge thereof to either the top or bottom surface of the airfoil body. The flexible strip has a spanwise length that is a function of the airfoil body's span, a chordwise width that is a function of the airfoil body's chord length, and a thickness that is a function of the airfoil body's maximum thickness.</p> |
申请公布号 |
WO2009032384(A2) |
申请公布日期 |
2009.03.12 |
申请号 |
WO2008US67075 |
申请日期 |
2008.06.16 |
申请人 |
UNITED STATES OF AMERICA AS REPRESENTED BY THE ADMINISTRATOR OF THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATION;SHAMS, QAMAR, A.;LIU, TIANSHU |
发明人 |
SHAMS, QAMAR, A.;LIU, TIANSHU |
分类号 |
B64C3/38 |
主分类号 |
B64C3/38 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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