03.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
NUMERICAL AND EXPERIMENTAL STRENGTH ANALYSIS OF LATTICE COMPOSITE FUSELAGE STRUCTURES
A. Dzuba¹, A. Shanygin¹, I. Kondakov¹, A. Razin², V. Vassiliev²; ¹Central Aerohydrodynamic Institute (TsAGI), Russia ;²Central Research Institute for Special Machinery (CRISM), Russia
The work is devoted to the validation of the methods and algorithms for solving new tasks of strength of lattice composite fuselage structures on the basis of comparative analysis of numerical analysis and experimental data. The experimental data was obtained during testing of static and cyclic strength of full-scale lattice composite fuselage barrel.
The agreement No. 14.628.21.0002 with the Russian Federation Ministry of Education and Science about granting subsidy, Project identification number RFMEFI62815X0002.