发明名称 A SUPERCRITICAL AEROFOIL
摘要 A supercritical aerofoil having a large leading edge radius of curvature, a radius of curvature over substantially the whole upper surface appreciably higher than the mean radius over the front half of the lower surface, a concave surface to the rear half of the lower surface, and a thickness/chord ratio of 10- 14%.
申请公布号 AU1169276(A) 申请公布日期 1977.09.08
申请号 AU19760011692 申请日期 1976.03.04
申请人 SECRETARY OF STATE FOR DEFENCE IN HER BRITANNIC MAJESTY@S;GOVERNMENT OF THE UNITED KINGDOM OF GREAT BRITAIN AND NORTHERN;IRELAND 发明人 JOHN LESLIE FULKER;DAVID JOHN HALL;ROBERT CHRISTOPHER LOCK
分类号 B64C3/14 主分类号 B64C3/14
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