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Information × Registration Number 0209U006030, 0106U001042 , R & D reports Title Experimental and theoretic substanation of aviation panel structures fatigue design procedure in condition of strain and bend. popup.stage_title Head Fomichev Petro, Registration Date 19-01-2009 Organization National Aerospace University named by N.E.Zhukovsky "Kharkov aviation institute" popup.description2 The longevity computation method for wing panels under the conditions of the cyclic stress-strain and bend using the local stress - strain state has been developed. In the capacity of source information the cyclic deformation and fatigue behaviors of the structural material have been used. Product Description popup.authors popup.nrat_date 2020-04-02 Close