发明名称 VLEUGEL VOOR EEN LUCHTVAARTUIG.
摘要 An airfoil having an upper surface shaped to control flow accelerations and pressure distribution over the upper surface and to prevent separation of the boundary layer due to shock wave formulation at high subsonic speeds well above the critical Mach number. A highly cambered trailing edge section improves overall airfoil lifting efficiency.
申请公布号 NL165423(B) 申请公布日期 1980.11.17
申请号 NL19720015161 申请日期 1972.11.09
申请人 NATIONAL AERONAUTICS AND SPACE ADMINISTRATION, WASHINGTON D.C. 发明人
分类号 B64C3/14;B64C23/00;B64C23/04 主分类号 B64C3/14
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