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All articles by "Mikhailovskiy K.V."
Key issues in creating inflatable braking devices for removal of the failed satellites into the atmosphere dense layers Part 3. Assessment of the shell resistance to impacts of micrometeorites and elements of small space debris
Authors: Reznik S.V., Mikhailovskiy K.V., Abramova E.N. | Published: 05.09.2023 |
Published in issue: #9(762)/2023 | |
Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
Keywords: space debris, inflatable braking device, polymer film, micrometeoroids, impact resistance, smoothed particle method |
Topological Optimization of the Strength Element of the Aircraft Compartment Made of Metal-Matrix Composite Material
Authors: Magidov I.S., Mikhailovskiy K.V. | Published: 25.12.2021 |
Published in issue: #1(742)/2022 | |
Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
Keywords: flight vehicle, direct laser growth, frame topological optimization, metal-matrix composite material |
Development of a Method for Determining Radiant Heat Transfer for Spacecraft Platforms in Near Earth Orbit Flight
Authors: Mikhailovskiy K.V., Gorodetskiy M.A. | Published: 19.02.2021 |
Published in issue: #3(732)/2021 | |
Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
Keywords: spacecraft platforms, heat fluxes, orbit parameters, orientation parameters, radiation flux, Earth albedo |
Accounting for Icing in the Design Analysis of Polymer Composite Wings
Authors: Mikhailovskiy K.V., Baranovski S.V. | Published: 12.03.2019 |
Published in issue: #3(708)/2019 | |
Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
Keywords: wing surface, ice covering, aerodynamic characteristics, ice accretion, aircraft icing |
Modeling the Heating of the Binder of Polymeric Composite Materials Using Microwave Radiation
Authors: Prosuntsov P.V., Reznik S.V., Mikhailovskiy K.V., Belenkov E.S. | Published: 24.12.2018 |
Published in issue: #12(705)/2018 | |
Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
Keywords: rocket and space technology, polymer composite material, binder curing, microwave radiation, representative volume element |
The Methods of Designing a Polymer Composite Wing Using Parametrical Modeling. Part III. Selection and Justification of Optimal Schemes for Reinforcing Load Bearing Elements
Authors: Mikhailovskiy K.V., Baranovski S.V. | Published: 31.05.2018 |
Published in issue: #5(698)/2018 | |
Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
Keywords: airliner, wing, structural arrangement, carbon fibre, reinforcement pattern |
The Methods of Designing a Polymer Composite Wing Using Parametrical Modeling. Part II. Design of the Load Bearing Structure
Authors: Mikhailovskiy K.V., Baranovski S.V. | Published: 16.12.2016 |
Published in issue: #12(681)/2016 | |
Category: Aviation, Rocket and Technology | |
Keywords: passenger jet, wing, polymer composite materials, structural arrangement, stringer, rib, longeron |
The Methods of Designing a Polymer Composite Wing Using Parametrical Modeling. Part 1. The Rationale for Selecting Wing Geometry and the Calculation of Airloads
Authors: Mikhailovskiy K.V., Baranovski S.V. | Published: 24.11.2016 |
Published in issue: #11(680)/2016 | |
Category: Aviation, Rocket and Technology | |
Keywords: airliner, wing, polymer composite materials, structural arrangement, airloads |