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The content and experience of implementing the direction of model-based development of rocket and space systems in specialized educational institutions
| Authors: Kabanov А.А., Fedorov I.A., Datsuk I.V. | Published: 06.11.2022 |
| Published in issue: #11(752)/2022 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
| Keywords: rocket and space systems, design process, model-based development, digital twins, ontological engineering, specialist training |
Comparative evaluation of tribotechnical characteristics of the W-S-N and W-S-C composition combined solid lubricating coatings of magnetron application for the normal atmospheric conditions
| Authors: Khopin P.N. | Published: 11.12.2022 |
| Published in issue: #12(753)/2022 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
| Keywords: solid lubricant coatings, magnetron application, tribotechnical characteristics, normal atmosphere |
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 |
Investigation of the drag of small-sized aircraft in the presence of a longitudinal central through channel
| Authors: Iljukhin S.N., Moskalenko V.O. | Published: 18.01.2023 |
| Published in issue: #1(754)/2023 | |
| Category: Aviation, Rocket and Technology | Chapter: Aerodynamics and Heat Transfer Processes in Aircraft | |
| Keywords: ballistic track, drag coefficient, through cylindrical channel, bullet of the Match |
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 |
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 |
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 |
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 |
Evaluation of the possibility to use composite material in the structure of the rocket stage cryogenic conical tank
| Authors: Ustinova A.P., Siuskina Yu.L., Peshkov R.A. | Published: 10.03.2023 |
| Published in issue: #3(756)/2023 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
| Keywords: cryogenic conical tank, composite materials, geodesic winding |
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 |