Virtual simulation of experiment at static trials of the aircraft primary structure panels
Автор: Dudarkov Yury Ivanovich, Limonin Mikhail Valeryevich, Naumov Sergey Mikhaylovich, Osipyan Evgeny Eduardovich
Журнал: Космические аппараты и технологии.
Рубрика: Космонавтика
Статья в выпуске: 1 (11), 2015 года.
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The results of virtual simulation of the experimental work for evaluation of loadbearing capacity of stringer panels of aircraft structure are presented. The modeling is based on the finite element method (FEM) by taking geometrical and physical nonlinearity into account. The experimental technique and principle of virtual modeling are shown. The numerical and test data comparison are presented.
Virtual simulation, stringer panel, local buckling failure, load-bearing capacity, fem, tension sensor
Короткий адрес: https://sciup.org/14117341
IDR: 14117341
