发明名称 Laminar flow wing for transonic cruise
摘要 In combination, an aircraft wing and fuselage, comprising the wing having camber at or near the wing leading edge which has blunted sharpness and low sweep angle, and the fuselage having indentation along the wing side thereof, and lengthwise of the fuselage.
申请公布号 US7000870(B2) 申请公布日期 2006.02.21
申请号 US20030693411 申请日期 2003.10.23
申请人 AERION CORPORATION 发明人 TRACY RICHARD R.;CHASE JAMES D.;KROO ILAN
分类号 B64C1/38;B64C3/14 主分类号 B64C1/38
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