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Promising solid lubricant coatings for use in the normal atmosphere and vacuum
| Authors: Khopin P.N. | Published: 09.07.2024 |
| Published in issue: #7(772)/2024 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
| Keywords: solid lubricant coatings, tribological characteristics, closed field method, unbalanced magnetron-ion sputtering, dry air, humid air |
Theoretical and numerical determination of the polymer composite material permeability by the multiscale simulation approach. Part 1. GFRP
| Authors: Prosuntsov P.V., Polskiy P.V. | Published: 13.08.2024 |
| Published in issue: #8(773)/2024 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: polymer composite material, fiberglass homogeneous characteristics, dielectric characteristics, representative volume element, multiscale simulation, electromagnetic radiation |
Geometric instability problems in monolithic products made of the carbon-based polymer composites
| Authors: Nekravtsev E.N., Safonov K.S., Oganesov V.A., Popov I.S., Samokhvalov V.V. | Published: 15.08.2024 |
| Published in issue: #8(773)/2024 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
| Keywords: polymer composite material, monolithic panel warping, carbon-based prepreg, autoclave technology, equilibrium laying scheme |
Design and development of an experimental setup for the hydrodynamic research
| Authors: Isaev A.I., Kudryavtsev A.A., Molokova S.V. | Published: 04.09.2024 |
| Published in issue: #9(774)/2024 | |
| Category: Aviation, Rocket and Technology | Chapter: Aerodynamics and Heat Transfer Processes in Aircraft | |
| Keywords: hydrodynamic research, experimental setup, hydro-flume, hydro-pool, flow visualization |
Determination of internal stresses arising in the structural elements heat-protective coating of the propulsion system at alterations in the ambient temperature
| Authors: Ushakova E.S., Tuponogov V.G. | Published: 14.09.2024 |
| Published in issue: #9(774)/2024 | |
| Category: Aviation, Rocket and Technology | Chapter: Aerodynamics and Heat Transfer Processes in Aircraft | |
| Keywords: solid fuel rocket engine, heat-protective coating, thermal cycling, numerical simulation, stress-strain state |
Methods in forcing a gas turbine engine
| Authors: Pismennyi V.L. | Published: 17.09.2024 |
| Published in issue: #9(774)/2024 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
| Keywords: gas turbine engine, stoichiometric engine, hypersonic aviation, hyperboost, turbine boost, turbojet engine, methods of boosting a gas turbine engine |
Justification of requirements to the process of organic glazing structural elements moulding using the pressure sintering
| Authors: Chechin D.E., Danilaev M.P., Petrachkov D.N. | Published: 11.10.2024 |
| Published in issue: #10(775)/2024 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
| Keywords: aviation glazing, optical distortions, moulding technology, monolithic polycarbonate, surface defects |
Orbital and ground control system reliability factors influencing the throughput of the multi-satellite orbital constellation ground control
| Authors: Potyupkin A.Y., Ruslekov A.A, Timofeev Y.A., Volko S.A. | Published: 13.11.2024 |
| Published in issue: #11(776)/2024 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
| Keywords: multi-satellite orbital constellation, throughput, equilibrium condition, ground control system |
Study of combustion processes using a bench on board the International Space Station
| Authors: Pichugin S.B. | Published: 14.11.2024 |
| Published in issue: #11(776)/2024 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
| Keywords: liquids and gases combustion, combustion processes, research bench, International Space Station |
Constructing a turbine blade damage accumulation model for accounting the long-term operating time
| Authors: Sapronov D.V., Khudyakova A.D., Semenov A.V., Kosovsky D.V., Selivanov A.N. | Published: 16.11.2024 |
| Published in issue: #11(776)/2024 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: damage accumulation model, turbine blade service life, operating time, long-term strength, material creep |