Shock-induced separation of airflow occurring symmetrically near the wing root of a sweptback wing may result in
a high-speed stall and sudden Pitchup due to the center of pressure moving forward on the wing.
severe porpoising due to an attempt to recover control while under reverse command.
a severe diving moment, due to the center of pressure moving aft on the wing and a decrease of downwash on the horizontal tail.
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