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All articles by "Reznik S.V."
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 |
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 |
Key issues of creating the inflatable braking devices for removal of the failed satellites into the atmosphere dense layers Part 2. Analysis of the thermal regime under the combined heating conditions
| Authors: Reznik S.V., Abramova E.N. | Published: 30.05.2023 |
| Published in issue: #6(759)/2023 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: space debris, nanosatellite removal, inflatable braking device, polymer films, temperature state simulation, thermal mode |
Key issues of creating the inflatable braking devices for removal of the failed satellites into the atmosphere dense layers Part 1. Conceptual design. Motion in the rarefied atmosphere
| Authors: Reznik S.V., Abramova E.N. | Published: 28.04.2023 |
| Published in issue: #5(758)/2023 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: space debris, near-Earth space cleanup, inflatable braking device, polymer films, rarefied atmosphere, motion simulation |
Nonlinear Analysis of the Reinforced Three-Layer Composite Panel sStrength
| Authors: Vasilchenko K.S., Reznik S.V., Smerdov A.A., Molodchikov S.E. | Published: 04.09.2021 |
| Published in issue: #10(739)/2021 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: three-layer structure, composite fracture, finite element modeling, fracture criterion, load-bearing capacity, nonlinear strength analysis |
An Experimental Study to Determine Mechanical and Thermophysical Characteristics of Thin-Walled Carbon Plastic Antenna Reflectors
| Authors: Novikov A.D., Reznik S.V., Denisov O.V. | Published: 05.03.2020 |
| Published in issue: #3(720)/2020 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: reflectors of space antennas, carbon fiber, experiment, elastic modulus, thermal conductivity |
Methods of Creating Functional Models of Gas Turbine Engine Parts by Means of Numerical Modeling and Machine Learning Algorithms Using a Turbine Disk as an Example
| Authors: Reznik S.V., Sapronov D.V., Vasilyev B.E., Semenov A.V. | Published: 26.11.2019 |
| Published in issue: #11(716)/2019 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: gas turbine engine, turbine disk, functional model, machine learning |
The Determination of Rational Parameters of Lock Joints of Ceramic Blades with a Metal Disk in Advanced Aircraft Gas Turbine Engines. Part II. Testing of the Rotor Model
| Authors: Reznik S.V., Sapronov D.V., Karimbaev T.D., Mezencev M.A. | Published: 23.07.2019 |
| Published in issue: #7(712)/2019 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: gas turbine engine, impeller, lock joint, ceramic blade |
The Determination of Rational Parameters of Lock Joints of Ceramic Blades with a Metal Disk in Advanced Aircraft Gas Turbine Engines. Part I. Models of Mechanical and Thermal Contact of Ceramic and Metal Parts of the Turbine Impeller
| Authors: Reznik S.V., Sapronov D.V., Karimbaev T.D., Mezencev M.A. | Published: 18.06.2019 |
| Published in issue: #6(711)/2019 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: gas turbine engine, lock joint, ceramic blades, contact interaction |
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 |