
Показано, что для обеспечения надежности элементов конструкции летательных аппаратов критерии сопротивления разрушению могут быть использованы на этапе проектирования.
It is shown that for fracture resistance criteria implementation while securing reliability of aircrafts structural components during design stage can be used.
НАДЕЖНОСТЬ ЭЛЕМЕНТОВ КОНСТРУКЦИИ, ВНЕЗАПНЫЕ И ПОСТЕПЕННЫЕ ОТКАЗЫ, СОПРОТИВЛЕНИЕ РАЗРУШЕНИЮ, ПОВРЕЖДЕНИЕ
НАДЕЖНОСТЬ ЭЛЕМЕНТОВ КОНСТРУКЦИИ, ВНЕЗАПНЫЕ И ПОСТЕПЕННЫЕ ОТКАЗЫ, СОПРОТИВЛЕНИЕ РАЗРУШЕНИЮ, ПОВРЕЖДЕНИЕ
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