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Digital Simulation Verification and Validation
| Authors: Salnikov A.V., Frantsuzov M.S., Vinogradov K.A., Pyatunin K.R., Nikulin A.S. | Published: 09.09.2022 |
| Published in issue: #9(750)/2022 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
| Keywords: verification and validation, mathematical model, computer simulation, digital twin, gas turbine engine |
Numerical Analysis of Corrugation Development during Oblique Compression of a Plate When Manufacturing Angle Metal Parts
| Authors: Boyarskiy D.S., Tarasov V.A., Baburin M.A., Baskakov V.D., Boyarskaya R.V. | Published: 27.08.2022 |
| Published in issue: #9(750)/2022 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
| Keywords: oblique compression, stability loss, corrugation magnitude, developing corrugation |
Optimal Costs for Combined Deorbiting Outsized Orbital Debris Using an Electric Propulsion Engine
| Authors: Golubek A.V. | Published: 29.06.2022 |
| Published in issue: #7(748)/2022 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
| Keywords: combined deorbiting, electric propulsion engine, energy costs |
Deviations from the Fourier Hypothesis, Detected during the Low Frequency Modal Analysis of the Box-Shell
| Authors: Arinchev S.V. | Published: 11.05.2022 |
| Published in issue: #6(747)/2022 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
| Keywords: separation of variables, Fourier hypothesis, frequency shift |
Empirical Evidence for Incorrectness of Using Separation of Variables according to the Fourier Method in Oscillation Theory
| Authors: Arinchev S.V. | Published: 21.04.2022 |
| Published in issue: #5(746)/2022 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
| Keywords: separation of variables, Fourier hypothesis, frequency shift |
Digital Twins — a Platform for Aircraft Engine Lifecycle Management
| Authors: Salnikov A.V., Gordin M.V., Shmotin Yu.N., Nikulin A.S., Makarov P.V., Frantsuzov M.S. | Published: 01.04.2022 |
| Published in issue: #4(745)/2022 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
| Keywords: digit twin, gas turbine engine, requirement matrix, digital platform, life cycle, mathematical modeling |
On the Friction Mechanisms and Assessment of Tribological Characteristics of Solid Lubricant Coatings of Various Application Methods
| Authors: Khopin P.N. | Published: 30.03.2022 |
| Published in issue: #4(745)/2022 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
| Keywords: solid lubricant coatings, magnetron-high-frequency application, tribotechnical characteristics, normal atmosphere |
Analysis of the Basic Design Parameters of a Small Upper Stage
| Authors: Malyh D.A., Peshkov R.A., Shalashov M.A. | Published: 23.03.2022 |
| Published in issue: #4(745)/2022 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
| Keywords: small upper stage, spacecraft, basic design parameters |
Analysis of the Main Methods of Obtaining Propellant by Electrolysis of Water
| Authors: Shalashov M.A., Peshkov R.A. | Published: 07.03.2022 |
| Published in issue: #3(744)/2022 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
| Keywords: oxygen-hydrogen propulsion system, onboard electrolysis unit, small spacecraft |
Approximate Methodology for Design Ballistic Calculation of Two-Stage Launch Vehicles
| Authors: Mukhamedov L.P., Kirievskii D.A. | Published: 27.01.2022 |
| Published in issue: #2(743)/2022 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
| Keywords: design ballistic calculation method, design ballistics problems, design ballistic parameters, launch vehicle, characteristic velocity losses |