Vladimir I. Tsimbalyuk, Tatiana I. Orlova, Kirill A. Mitenkov

DOI Number: N/A

Conference number: IFASD-2015-135

The contribution of the stages of flight with appreciable separated flows (a flaps extension and a slowdown by spoilers) in a cumulative fatigue damage of an airframe is demonstrated. Possibilities of the vibrations suppression caused by separated flows are shown. The results of analytical and experimental researches to increase the fatigue characteristics of an aircraft by means of loads alleviation system are described. Capabilities of loads exceedances reduction during ground operations by optimization of shock absorption characteristics are shown.

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