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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 |
Experimental study of the propulsion system demonstrator with a central body
Authors: Vaulin S.D., Salich V.L., Erpalov A.V., Schulz A.O., Khoroshevskii K.A., Khazhiakhmetov K.I. | Published: 25.11.2023 |
Published in issue: #12(765)/2023 | |
Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
Keywords: propulsion system, rocket engine, central body, experimental modal analysis, demonstrator vibration state, acoustic impact |
Pipe manufacture by sheet blank rolling
Authors: Lozovskiy I.V., Mariin S.B., Chernomas V.V., Kuznetsov A.K. | Published: 02.12.2023 |
Published in issue: #12(765)/2023 | |
Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
Keywords: pipes and profiles manufacture, aircraft, sheet blank rolling, elastic loose medium |
Two-Phase Dual–Axis Model of a Multihop System with Differentiated Transmission Capacity of its Subscriber and Inter-Satellite Links
Authors: Pichugin S.B. | Published: 06.12.2023 |
Published in issue: #12(765)/2023 | |
Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
Keywords: subscriber and inter-satellite links, multihop communication system, on-board router, queuing system, simplest flow |
Determination of the thermal battery effective thermal conductivity by the parametric identification methods
Authors: Borschev N.O. | Published: 27.12.2023 |
Published in issue: #1(766)/2024 | |
Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
Keywords: phase transition, thermal regime support system, conjugate directions method, iterative regularization method |
High-temperature absorbing coatings for ground thermal testing of the structural elements of the high-speed aircrafts at the radiation heating benches
Authors: Fokin V.I., Terekhin A.V., Rajlyan V.S. | Published: 07.02.2024 |
Published in issue: #2(767)/2024 | |
Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
Keywords: ground testing, radiation heating, quartz halogen lamps, high-temperature coating, absorptivity |
Selecting optimal design parameters for a thermal control system of the lithium-ion battery
Authors: Borschev N.O. | Published: 19.03.2024 |
Published in issue: #4(769)/2024 | |
Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
Keywords: axial heat pipe, radiating emitter, conjugate direction method, thermal control system |
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 |
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 |
Analyzing thermal state of the Buran orbital space vehicle structure in the areas of possible damages to its thermal protection elements
Authors: Timoshenko V.P., Prosuntsov P.V., Reznik S.V. | Published: 10.06.2024 |
Published in issue: #6(771)/2024 | |
Category: Aviation, Rocket and Technology | Chapter: Aerodynamics and Heat Transfer Processes in Aircraft | |
Keywords: thermal protection, fibrous ceramics, felt substrate, thermal conductivity coefficient, thermal destruction, metal skin melting |