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Stress–strain analysis of a thin-shell part of fuselage using a triangular finite element with lagrange multipliers
Klochkov Y.V., Nikolaev A.P., Vakhnina O.V., Kiseleva T.A.
Study of the Local Strength of the Main Rotor Torsion Bar under the Action of Flight and Test Bench Loads
Mitryaikin V.I., Shuvalov V.A.
Effect of a Model and Boundary Conditions on the Results of Analyzing the Stress-Strain State of a Low-Pressure Compressor Rotor
Arkhipov A.N., Volgina M.V., Matushkin A.A., Ravikovich Y.A., Kholobtsev D.P.
Analysis of structural elements made of composite materials with defects
Kokurov A.M., Odintsev I.N.
Nonlinear Deformation and Stability of Discrete-Reinforced Elliptical Cylindrical Composite Shells under Torsion and Internal Pressure
Zheleznov L.P., Kabanov V.V., Boiko D.V.
Analysis of the Impact of Fan Blade Geometric Deviations on the Strength Properties
Arkhipov A.N., Volgina M.V., Matushkin A.A., Ravikovich Y.A., Kholobtsev D.P.
Research on Nonlinear Deformation and Stability of an Advanced Aircraft Fuselage Composite Section under Pure Bending
Belov V.K., Zheleznov L.P., Ognyanova T.S.
Probabilistic Assessment of Life for Gas Turbine Engine Parts Considering Manufacture Tolerances
Arkhipov A.N., Volgina M.V., Matushkin A.A., Ravikovich Y.A., Kholobtsev D.P.
Numerical Estimation of Weight Efficiency for Aircraft Composite Lattice Shells with Grid Parameter Variable over Height
Bokuchava P.N., Evstaf’ev V.A., Babuk V.A.
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