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fbtwitterlinkedinvimeoflicker grey 14rssslideshare1
Publisher: National Aviation University
Languages: Ukrainian
Types: Unknown
Subjects:
 The features of a task of optimization of the plane with unmanned completely wing are considered the existing approaches the block diagram of mathematical model of the plane with unmanned completely wing is given in the decision of similar tasks.  Рассмотрены особенности задачи оптимизации самолета с сочлененным тандемным крылом и подходы к решению аналогичных задач. Приведена структурная схема математической модели самолета с сочлененным тандемным крылом.  Розглянуто особливості задачі оптимізації літака зі зчленованим тандемним крилом і підходи до розв’язання аналогічних задач. Наведено структурну схему математичної моделі літака зі зчленованим тандемним крилом.
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