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Force method application in calculating spatial motion of a manipulator with the massive solid body taking into account the links and rotary drives elasticity
| Authors: Grishanina T.V., Russkikh S.V., Shklyarchuk F.N. | Published: 07.11.2023 |
| Published in issue: #11(764)/2023 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: hand-type manipulator, spatial motion dynamics, elastic vibrations |
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 |
Key issues in creating inflatable braking devices for removal of the failed satellites into the atmosphere dense layers Part 3. Assessment of the shell resistance to impacts of micrometeorites and elements of small space debris
| Authors: Reznik S.V., Mikhailovskiy K.V., Abramova E.N. | Published: 05.09.2023 |
| Published in issue: #9(762)/2023 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: space debris, inflatable braking device, polymer film, micrometeoroids, impact resistance, smoothed particle method |
Methods and techniques used in increasing gas temperature in front of the gas turbine engine turbine
| Authors: Pismennyi V.L. | Published: 05.06.2023 |
| Published in issue: #6(759)/2023 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: heat resistance of materials, blade cooling, gas temperature, circulating heat exchanger, heat-shielding coatings, gas turbine engine, air-liquid cooling |
Key issues of creating the inflatable braking devices for removal of the failed satellites into the atmosphere dense layers Part 2. Analysis of the thermal regime under the combined heating conditions
| Authors: Reznik S.V., Abramova E.N. | Published: 30.05.2023 |
| Published in issue: #6(759)/2023 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: space debris, nanosatellite removal, inflatable braking device, polymer films, temperature state simulation, thermal mode |
Plane motion dynamics of a space-based crane-manipulator of the arm type taking into account the links’ bending
| Authors: Russkikh S.V., Shklyarchuk F.N. | Published: 10.05.2023 |
| Published in issue: #5(758)/2023 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: crane-manipulator of the arm type, plane motion dynamics, elastic oscillations, equations in generalized coordinates |
Key issues of creating the inflatable braking devices for removal of the failed satellites into the atmosphere dense layers Part 1. Conceptual design. Motion in the rarefied atmosphere
| Authors: Reznik S.V., Abramova E.N. | Published: 28.04.2023 |
| Published in issue: #5(758)/2023 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: space debris, near-Earth space cleanup, inflatable braking device, polymer films, rarefied atmosphere, motion simulation |
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 |
Methods for controlling temperature of the instrumentation equipment using the contour heat pipe
| Authors: Borschev N.O. | Published: 02.03.2023 |
| Published in issue: #3(756)/2023 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: contour heat pipe, compensation cavity, thermal control systems |
Selection and optimization of a promising structural power scheme for the unmanned aerial vehicle fuselage made of polymer composite materials
| Authors: Baranovski S.V., Khaing Phyo Zaw | Published: 02.03.2023 |
| Published in issue: #3(756)/2023 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: fuselage, structural power structure, anisogrid design, auxetic design, biosimilar design, parametric optimization |