
A multilevel flowchart for solving optimization problems of design of composite and metallic structures under strength, stiffness, buckling and aero-elasticity constraints is presented. It has been implemented in the framework of the software for multidisciplinary structural optimization. A set of test problems has been solved and the multilevel approach has been used in design studies of advanced aircraft structures.
Представлена многоуровневая процедура решения задач оптимизации конструкций с учетом ограничений по прочности, жесткости, устойчивости и аэроупругости, реализованная в рамках программного обеспечения многодисциплинарного проектирования. Процедура опробована на решении ряда задач проектирования элементов авиационных конструкций.
МНОГОДИСЦИПЛИНАРНАЯ ОПТИМИЗАЦИЯ КОНСТРУКЦИЙ, МНОГОУРОВНЕВЫЙ ПОДХОД, МЕТОД КОНЕЧНЫХ ЭЛЕМЕНТОВ, МЕТОД ЗАДАННЫХ ФОРМ, НАПРЯЖЕНИЕ, ПОТЕРЯ УСТОЙЧИВОСТИ, АЭРОУПРУГОСТЬ
МНОГОДИСЦИПЛИНАРНАЯ ОПТИМИЗАЦИЯ КОНСТРУКЦИЙ, МНОГОУРОВНЕВЫЙ ПОДХОД, МЕТОД КОНЕЧНЫХ ЭЛЕМЕНТОВ, МЕТОД ЗАДАННЫХ ФОРМ, НАПРЯЖЕНИЕ, ПОТЕРЯ УСТОЙЧИВОСТИ, АЭРОУПРУГОСТЬ
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