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Simulation of Small-Size Space Debris Impact on the Protective Shield of a Transformable Trap
| Authors: Prosuntsov P.V., Alekseev A.A., Zherebtsova E.O. | Published: 28.10.2021 |
| Published in issue: #11(740)/2021 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: spacecraft, space debris, spacecraft shielding, composite materials, hypervelocity impact, Smooth Particle Hydrodynamics |
Multicriteria Optimization of Composite Wing of an Unmanned Aircraft
| Authors: Lin Aung Naing, Tatarnikov O.V., Wai Aung Phyo | Published: 28.10.2021 |
| Published in issue: #11(740)/2021 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: unmanned aircraft, composite wing, load-bearing frame, double-tee spars, wing top skin, bottom skin, multicriteria optimization |
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 |
Nonlinear Analysis of the Reinforced Three-Layer Composite Panel sStrength
| Authors: Vasilchenko K.S., Reznik S.V., Smerdov A.A., Molodchikov S.E. | Published: 04.09.2021 |
| Published in issue: #10(739)/2021 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: three-layer structure, composite fracture, finite element modeling, fracture criterion, load-bearing capacity, nonlinear strength analysis |
Design Optimization of Shape and Layup Sequence of Polymer Composite Load Bearing Elements of Light Aircraft
| Authors: Tun Lin Htet, Prosuntsov P.V. | Published: 20.08.2021 |
| Published in issue: #9(738)/2021 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: tail section, fuselage, load bearing ribs, parametric optimization, topological optimization method, mass reducing, structural layout |
Wing Shape Optimization and Selecting Rational Re-Entry Trajectory for Reusable Spacecraft of Tourist Class
| Authors: Ashikhmina E.R., Prosuntsov P.V. | Published: 23.07.2021 |
| Published in issue: #8(737)/2021 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: reusable spacecraft, space tourism, trajectory control, re entry trajectory design, shape optimization |
Multi-Criteria Optimization of a Two-Spar Composite Wing for a Light Aircraft
| Authors: Tatarnikov O.V., Phyo W.A., Naing Lin Aung | Published: 15.04.2021 |
| Published in issue: #5(734)/2021 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: composite wing, multi-criteria optimization, optimization criteria, optimization parameters of the wing, the geometrically nonlinear model |
Development of a Method for Determining Radiant Heat Transfer for Spacecraft Platforms in Near Earth Orbit Flight
| Authors: Mikhailovskiy K.V., Gorodetskiy M.A. | Published: 19.02.2021 |
| Published in issue: #3(732)/2021 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: spacecraft platforms, heat fluxes, orbit parameters, orientation parameters, radiation flux, Earth albedo |
Analysis of the Anisotropic Heat-Protective Material Application Effectiveness in the Implementation of Trajectories with Multiple Re-entries into the Atmosphere
| Authors: Leonov V.V., Zarubin V.S., Ayrapetyan M.A. | Published: 26.01.2021 |
| Published in issue: #2(731)/2021 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: Moon exploration, glide descent craft, multiple re-entries into the atmosphere, thermal protection coating, anisotropic heat-protective materials |
An Analysis of Combined Radiation-Conductive Heat Transfer During the Destruction of Porous Carbon-Ceramic Composite Material of the Thermal Protection Shield
| Authors: Prosuntsov P.V., Barinov D.Y. | Published: 13.12.2020 |
| Published in issue: #12(729)/2020 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: mathematical model, descent module, thermal protection, radiation- conductive heat transfer |