| 摘要 |
Improved supersonic laminar flow wing structure, on a supersonic aircraft , having one or more of the following: strake extending forwardly of the win g inboard extent, raked wing tip, reversed fillet at strake or fuselage junc tion, inboard leading edge flap extending over less than about 15 % of the i nboard wing panel span, hybrid plain-split flap having a lower surface porti on deflectable downwardly relative to plain flap extent.
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