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I beg to differ Gust response at high subsonic speed/low altitude also requires high sweep (decreases the CL alpha). Structurally, the delta wing offers a lot of absolute thickness for a given airfoil thickness-to-chord to embed a large diameter fan.
I beg to differ
Gust response at high subsonic speed/low altitude also requires high sweep (decreases the CL alpha). Structurally, the delta wing offers a lot of absolute thickness for a given airfoil thickness-to-chord to embed a large diameter fan.