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The study of the aerodynamics of different configurations of aircraft with joined wing using panel-vortex method of symmetrical features (PANSIM). Performing the calculation and rating of the configurations aircraft with joined wing with a combination of different types of bearing surfaces.For each layout of the aircraft with joined wing was determined the effect relative impact of location and V-similarity angle the front wing on the transport aircraft efficiency and its corresponding prime aerodynamic lift coefficient value; on the maximum aerodynamic qualities and the corresponding optimal aerodynamic lift coefficient value.To select the optimal layout of aircraft with joined wing advisable to take the maximum transport efficiency values and maximum aerodynamic quality for distance between the front and rear wing aircraft.Due to the lack of information on the impact of combinations of bearing surfaces aircraft with joined wing on the aerodynamic performance and transport efficiency aircraft have been proposed recommendations of the aerodynamic design of aircraft with joined wing in which the aircraft will have a maximum range and flight duration.Detect the effect of the combinations of bearing surfaces aircraft with joined wing on the transport aircraft efficiency.Found rational construction layout construction solutions aircraft with joined wing., Исследуется аэродинамика различных компоновок летательных аппаратов с замкнутой пространственной системой крыльев с помощью панельно-вихревого метода симметричных особенностей (PANSIM). Выполняется расчет и оценка компоновок ЛА замкнутой пространственной схемы с различными типами соединения несущих поверхностей., Досліджується аеродинаміка різних компоновок літальних апаратів із замкненою просторовою системою крил за допомогою панельно-вихрового методу симетричних особливостей (PANSIM). Виконується розрахунок і оцінка компоновок ЛА замкненої просторової схеми з різними типами сполучення несучих поверхонь.

Досліджується аеродинаміка різних компоновок літальних апаратів із замкненою просторовою системою крил за допомогою панельно-вихрового методу симетричних особливостей (PANSIM). Виконується розрахунок і оцінка компоновок ЛА замкненої просторової схеми з різними типами сполучення несучих поверхонь. The study of the aerodynamics of different configurations of aircraft with joined wing using panel-vortex method of symmetrical features (PANSIM). Performing the calculation and rating of the configurations aircraft with joined wing with a combination of different types of bearing surfaces. For each layout of the aircraft with joined wing was determined the effect relative impact of location and V-similarity angle the front wing on the transport aircraft efficiency and its corresponding prime aerodynamic lift coefficient value; on the maximum aerodynamic qualities and the corresponding optimal aerodynamic lift coefficient value. To select the optimal layout of aircraft with joined wing advisable to take the maximum transport efficiency values and maximum aerodynamic quality for distance between the front and rear wing aircraft. Due to the lack of information on the impact of combinations of bearing surfaces aircraft with joined wing on the aerodynamic performance and transport efficiency aircraft have been proposed recommendations of the aerodynamic design of aircraft with joined wing in which the aircraft will have a maximum range and flight duration. Detect the effect of the combinations of bearing surfaces aircraft with joined wing on the transport aircraft efficiency. Found rational construction layout construction solutions aircraft with joined wing. Исследуется аэродинамика различных компоновок летательных аппаратов с замкнутой пространственной системой крыльев с помощью панельно-вихревого метода симметричных особенностей (PANSIM). Выполняется расчет и оценка компоновок ЛА замкнутой пространственной схемы с различными типами соединения несущих поверхностей.