| 发明名称 |
SPANWISE TAILORING OF DIVERGENT TRAILING EDGE WINGS |
| 摘要 |
A method for forming a transonic wing that segregates a baseline transon ic wing into a plurality of airfoil segments that are collectively modified an optimized so as to tailor a spanwise variation of the baseline transonic wing in a manner that includes the optimized airfoil segments. An improved wing is also provided.< /SDOAB>
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| 申请公布号 |
CA2430107(A1) |
申请公布日期 |
2003.12.20 |
| 申请号 |
CA20032430107 |
申请日期 |
2003.05.27 |
| 申请人 |
THE BOEING COMPANY |
发明人 |
PITERA, DAVID M.;GREGG, ROBERT D., III;VASSBERG, JOHN CHARLES |
| 分类号 |
B64C3/14;(IPC1-7):B64C3/10 |
主分类号 |
B64C3/14 |
| 代理机构 |
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代理人 |
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