发明名称 Slotted high lift aerofoils
摘要 A slotted aerofoil configuration is provided in which the leading element thereof is contoured to provide mild stall characteristics. A wing based partially or fully on such an aerofoil, an air vehicle including such wings, and a method for designing an aerofoil are also disclosed
申请公布号 US2007278354(A1) 申请公布日期 2007.12.06
申请号 US20070802964 申请日期 2007.05.29
申请人 ISRAEL AEROSPACE INDUSTRIES LTD. 发明人 SHEPSHELOVICH MICHAEL;NAGEL ALEX
分类号 B64C9/32 主分类号 B64C9/32
代理机构 代理人
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