FIELD: aeronautical engineering.
SUBSTANCE: each outer panel of proposed wing includes wing extension with sweep-back leading edge, root section with swept-forward leading edge and trailing edge; swivel part of wing outer panel is articulated with this section relative to vertical axis of flying vehicle; it may be turned backward in way of flow so that sweep angle of leading edge may change from initial swept-forward to swept-back magnitudes.
EFFECT: increased critical velocity of aero-elastic divergence.
2 dwg
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