Estimation of plane’s blade marginal states
Автор: Makhutov N.A., Moskvichev V.V., Seregin A.S., Stepanov M.N.
Журнал: Сибирский аэрокосмический журнал @vestnik-sibsau
Рубрика: Авиационная и ракетно-космическая техника
Статья в выпуске: 1-1 (22), 2009 года.
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The main types of plane' s blade marginal states are considered. Experimental calculated estimation of the retained strength and blade life time at static and cyclic loading are calculated. The ultimate and permissible dimension of cracks are determined. The calculated exhaust curves are received. It let make a conclusion about safety life time factor with the initial malfunction availability.
Exhaust safety, blades, constructions, planes
Короткий адрес: https://sciup.org/148175816
IDR: 148175816
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