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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 |
Method of designing the composite load-bearing elements of the fuselage tail section
| Authors: Tun Lin Htet, Prosuntsov P.V. | Published: 09.02.2023 |
| Published in issue: #2(755)/2023 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: light aircraft, fuselage tail section, power structure, parametric optimization, topological optimization, polymer composite material |
Thermal mathematical model of a two-phase circuit with mechanical pump and thermal hydraulic accumulator
| Authors: Borschev N.O. | Published: 27.01.2023 |
| Published in issue: #2(755)/2023 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: heat pipe, convective heat transfer, two-phase boiling coolant |
Interaction between the attacking drones salvo and the anti-aircraft drones salvo as a computer antagonistic non-Newtonian 2D game
| Authors: Arinchev S.V. | Published: 01.01.2023 |
| Published in issue: #1(754)/2023 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: drone salvo, non-Newtonian elastic element, 2D game |
Eight-channel frequency-response test of the cylindrical-shell-and-ring assembly in the range 1000 to 8000 Hz
| Authors: Arinchev S.V. | Published: 18.10.2022 |
| Published in issue: #11(752)/2022 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: detonation jet propulsion, Auger effect, Fourier hypothesis |