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
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