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All articles by "Zheleznov L.P."
Investigation of nonlinear deformation and stability of an elliptical cylindrical composite shell under axial compression
| Authors: Zheleznov L.P. | Published: 12.01.2026 |
| Published in issue: #1(790)/2026 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: elliptical cylindrical shells, polymer composite materials, nonlinear deformation, stability, finite element method, axial compression, weight efficiency |
Investigation of the stability of anisogrid circular cylindrical shells under combined loading by transverse force and internal pressure
| Authors: Zheleznov L.P. | Published: 14.11.2025 |
| Published in issue: #11(788)/2025 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: transverse bending, internal pressure, cylindrical composite shells, nonlinear deformation, stability, finite element method |
Nonlinear deformation and stability of the anisogrid circular cylindrical shells under transverse bending
| Authors: Zheleznov L.P. | Published: 23.09.2025 |
| Published in issue: #9(786)/2025 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: cylindrical composite shells, transverse bending, nonlinear deformation, shell stability, finite element method |
Nonlinear deformation and stability of a composite non-circular cylindrical shell exposed to torsion
| Authors: Zheleznov L.P. | Published: 03.12.2024 |
| Published in issue: #12(777)/2024 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: non-circular cylindrical shell, polymer composite materials, nonlinear deformation, shell stability, torsion, weight efficiency |
Study of nonlinear deformation and stability of the non-circular composite cylindrical shell exposed to loading with the bending moment
| Authors: Zheleznov L.P. | Published: 21.05.2024 |
| Published in issue: #6(771)/2024 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: non-circular cylindrical shells, polymer composite materials, nonlinear deformation, finite element method, bending moment, weight efficiency |
Investigation of nonlinear deformation and stability of a composite cylindrical shell under combined loading with torque, edge transversal force and internal pressure
| Authors: Zheleznov L.P. | Published: 10.10.2023 |
| Published in issue: #10(763)/2023 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: composite cylindrical shell, polymer composite materials, nonlinear deformation, shell stability, internal pressure, weight efficiency |
Research on the synthesis of bionic thin-walled structures of the aircraft fuselage compartment type
| Authors: Zheleznov L.P., Laperdina N.A. | Published: 21.03.2023 |
| Published in issue: #4(757)/2023 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: topological optimization, bionic structures, fuselage compartment stability, stress-strain state, factor of assurance, aircraft |
Nonlinear Deformation and Stability of a Composite Cylindrical Shell under a Combined Loading by a Bending Moment and an Edge Transverse Force
| Authors: Zheleznov L.P. | Published: 27.07.2022 |
| Published in issue: #8(749)/2022 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: cylindrical composite shells, polymer composite materials, nonlinear deformation, buckling mode, finite element method |
Study of the Effect of the Monolayers Stacking Sequence on the Composite cCylindrical Shell Stability
| Authors: Zheleznov L.P. | Published: 22.12.2021 |
| Published in issue: #1(742)/2022 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: cylindrical shells, polymer composite materials, nonlinear deforming, shell stability, finite element method |
Research on Nonlinear Deformation and Stability of an Aircraft Fuselage Composite Section under Transverse Bending
| Authors: Zheleznov L.P., Seriosnov A.N. | Published: 14.09.2021 |
| Published in issue: #10(739)/2021 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: cylindrical composite shells, nonlinear deformation, shall stability, finite element method |