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Combined effect of the climatic factors and impact damage on strength of the polymer composite plates
| Authors: Mitryaykin V.I., Bezzametnov O.N., Kuznetsov M.E., Nosov D.A., Tazhibaeva A.V. | Published: 18.07.2025 |
| Published in issue: #7(784)/2025 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: polymer composite materials, climatic testing, non-destructive testing, impact damage, plate strength |
Study of the physico-thermomechanical properties of the Ti-4.25Al-2V dispersion-hardened metal ceramics with SiC addition manufactured by the direct laser growing
| Authors: Magidov I.S., Mikhailovskiy K.V., Shalnova S.A., Klimova-Korsmik O.G. | Published: 02.06.2025 |
| Published in issue: #6(783)/2025 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: direct laser growing, additive technologies, metal ceramics, dispersion hardening, characteristics mathematical simulation |
Study of residual stresses in the annular plates used in the aerial vehicles
| Authors: Velikanov N.L., Sharkov O.V. | Published: 08.04.2025 |
| Published in issue: #4(781)/2025 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: aircraft, bimetallic annular plate, stress state, mathematical model, plate tension |
Theoretical and numerical determination of the polymer composite material permeability by the multiscale simulation approach. Part 2. GFRP
| Authors: Prosuntsov P.V., Polskiy P.V. | Published: 09.03.2025 |
| Published in issue: #3(780)/2025 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: polymer composite material, fiberglass homogeneous characteristics, dielectric characteristics, representative volume element, multiscale simulation, electromagnetic radiation |
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 |
Overview: computational and experimental research in studying acoustics and acoustic strength of the flying vehicles
| Authors: Khodina A.S. | Published: 18.11.2024 |
| Published in issue: #11(776)/2024 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: acoustic strength, vibroacoustic loads, sound insulation, full-scale testing, mathematical simulation |
Constructing a turbine blade damage accumulation model for accounting the long-term operating time
| Authors: Sapronov D.V., Khudyakova A.D., Semenov A.V., Kosovsky D.V., Selivanov A.N. | Published: 16.11.2024 |
| Published in issue: #11(776)/2024 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: damage accumulation model, turbine blade service life, operating time, long-term strength, material creep |
Theoretical and numerical determination of the polymer composite material permeability by the multiscale simulation approach. Part 1. GFRP
| Authors: Prosuntsov P.V., Polskiy P.V. | Published: 13.08.2024 |
| Published in issue: #8(773)/2024 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: polymer composite material, fiberglass homogeneous characteristics, dielectric characteristics, representative volume element, multiscale simulation, electromagnetic radiation |
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 |
Cooling capacity parametric identification of the two-stage cryostat nitrogen and helium stages
| Authors: Borschev N.O. | Published: 22.04.2024 |
| Published in issue: #5(770)/2024 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: heat transfer problem, iterative regularization method, stage cooling capacity, two-stage cryostat, conjugate directions method |