In a jet aircraft, the supersonic air flowing past the leadi…
In a jet aircraft, the supersonic air flowing past the leading edge of the wing generates far more lift than the subsonic air aft of the shock wave. At this point, your center of lift is located at the leading edge of your wing. As you speed up, that shockwave moves [blank1]. The high-lift region follows it [blank2], and the the center of lift moves [blank3], as well.
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