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For example, the main wing with small aspect ratio and medium sweep angle.
Well known.
This kind of aerodynamic layout is basically aimed at the unification of the maximum lift coefficient at low speeds, the lift-to-drag ratio at sub-transonic speeds, and the drag coefficient at supersonic speeds.
Good ideas.
But there are many problems in it.
Tang Rui doesn't think that Shen Huoyi has solved the problem.
But these issues are not fo ...
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