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Theoretical and experimental study of thermal conductivity and operational limits of a sodium axial heat pipe relative to the gravity vector orientation
| Authors: Borschev N.O., Kochegarova A.V. | Published: 31.07.2026 |
| Published in issue: #8(797)/2026 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: axial heat pipe, boiling limit, sonic limit, viscous limit, capillary limit |
Modelling of CubeSat satellite motion with inflatable braking device. Part 1. Determination of aerodynamic characteristics and trajectory parameters
| Authors: Guselnikov A.V., Fedyunina E.R., Prosuntsov P.V. | Published: 28.07.2026 |
| Published in issue: #8(797)/2026 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: microsatellite CubeSat, drag force, free-molecular flow, inflatable braking device, direct Monte Carlo simulation method |
Mathematical modeling of the thermal condition of pressurized aircraft compartments
| Authors: Nikolayev V.N. | Published: 16.04.2026 |
| Published in issue: #4(793)/2026 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: thermal state of the compartment, mathematical model, parabolic boundary value problem, discontinuous coefficients, integral averaging, stochastic differential equations |
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 |
Numerical modeling of the stress-strain state of a ceramic plate under impact loading
| Authors: Tatarnikov O.V., Rogov D.A., Prasolov A.N. | Published: 17.12.2025 |
| Published in issue: #12(789)/2025 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: impact loading, ceramic plate, dynamic stress-strain state, spall strength, finite element model |
Evaluation of the influence of yield conditions J2–J3 on the stress state of tubular specimens to confirm the static strength of gas turbine shafts
| Authors: Khudyakova A.D., Sapronov D.V., Babinets I.S., Kuryshev I.M. | Published: 17.11.2025 |
| Published in issue: #11(788)/2025 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: yield condition J2–J3, third invariant, plastic flow, type of stress state, Lode parameter, tangential rigidity |
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 |
Parameter optimization of a light aircraft wing made of the polymer composite material and analysis of the possible appearing defects. Part I. Computation of the optimal structural and power scheme
| Authors: Wai Yan Oo, Mikhailovskiy K.V. | Published: 12.09.2025 |
| Published in issue: #9(786)/2025 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: light sports aircraft, parametric optimization, structural and power scheme, polymer composite materials, stress-strain state, optimization criteria |
Development of a concentrated radiation heating facility for testing the high-temperature composite materials
| Authors: Khudorozhko M.V., Prosuntsov P.V. | Published: 19.08.2025 |
| Published in issue: #8(785)/2025 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: high-temperature composite materials, halogen lamp, radiation heating bench, concentrated radiation source, elliptical reflector, radiation heat exchange simulation |