发明名称 Spanwise tailoring of a trailing edge wedge to a wing
摘要 A method for forming a trailing edge wedge for a wing wherein the size and configuration of a trailing edge wedge at various points along the span of the trailing edge wedge are adjusted and analyzed in an iterative manner to form an improved trailing edge wedge. An improved wing assembly is also provided.
申请公布号 US2004135032(A1) 申请公布日期 2004.07.15
申请号 US20020175612 申请日期 2002.06.20
申请人 GREGG ROBERT D;VASSBERG JOHN CHARLES;PITERA DAVID M 发明人 GREGG ROBERT D;VASSBERG JOHN CHARLES;PITERA DAVID M
分类号 B64C3/10;B64C3/14;(IPC1-7):B64C1/00;B64C3/00;B64C5/00 主分类号 B64C3/10
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