A mathematical model, allowing to get an algorithm and method of calculation of aerodynamic descriptions of fine profile in the non-stationary nonlinear raising of task, is examined. Application of model allows to define the features of physics of the phenomena and probed processes, and also purposefully to probe the processes of flowing around of wings of eventual scope.
aircraft, type, model
"Matematycheskoe modelyrovanye obtekanyia profylia" [Mathematical modeling of flow profile],
Science and Technology of the Air Force of Ukraine,