The work was carried out by order of OJSC Tupolev, 2003.

Modeling the release of the flap, taking into account the dynamics of the "wing + flap + harvesting-release mechanism + external environment" in three-dimensional space. Main features of the model: elastic wing model; elastic flap model; non-stationary aerodynamic impact on the wing and flap; joint movement of 4 mechanisms of release-cleaning of the flap.

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