A Wedge witha Heat-Resistant Lining in a High-Speed Airflow: Comparative Estimate of the Thermal State
| Authors: Aliev Az.A., Zimin V.N. , Tovstonog V.A., Tomak V.I. | Published: 01.04.2022 |
| Published in issue: #1(140)/2022 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: aircraft, aerodynamic heating, thermal protection, thermal condition, heat-resistant material | |
Thermal State of an Aircraft Aerofoil in a High-Velocity Air Flow
| Authors: Aliev Az.A., Burkov A.S., Tovstonog V.A., Tomak V.I., Yagodnikov D.A. | Published: 05.09.2021 |
| Published in issue: #3(138)/2021 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: aerodynamic heating, thin aerofoil, oxidising atmosphere, thermal protection, refractory materials, oxides | |
Estimating the Thermal State and Methodological Issues in Gas Dynamic Testing of Refractory Ceramic Samples
| Authors: Tovstonog V.A., Tomak V.I., Burkov A.S. | Published: 23.12.2020 |
| Published in issue: #6(135)/2020 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: high-temperature gas flow, refractory ceramics, thermal state, physical simulation | |
Error Inherent in Simulating Planetary Thermal Effect on the Spacecraft Surface by using Isotropic Planetary Radiation Intensity Field Model Instead of Anisotropic
| Authors: Kolesnikov A.V., Pronina P.F., Paleshkin A.V. | Published: 23.12.2020 |
| Published in issue: #6(135)/2020 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: planet, radiation, radiation intensity field model, heat flux, angle factor, radiation field simulation, spacecraft | |
Method for Computational Estimation of Frost Resistance in Aircraft Paint Coatings
| Authors: Aliyev A.A., Аmpilogov A.Yu. | Published: 06.06.2020 |
| Published in issue: #3(132)/2020 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: ice accretion, coating, microre-lief, fatigue, computation, frost resistance, fracturing | |
Comparative Assessment of Thermal Protective Characteristics of Metal and Ceramic Shields of Flow Paths of High-Temperature Gas Dynamic Facilities
| Authors: Tovstonog V.A. | Published: 30.04.2020 |
| Published in issue: #2(131)/2020 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: gas dynamic facilities, high temperatures, thermal protection, metal shields, high-temperature ceramics, volume-reflecting scattering materials | |
Experimental Estimation of the Degree to which Samples of a 3d Material are able to Withstand Constant Compression Loading at High Temperatures
| Authors: Mostovoy G.E., Karpov A.P., Protsenko A.K., Shishkov I.V. | Published: 02.10.2018 |
| Published in issue: #5(122)/2018 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: creep, pitch, carbon-carbon composite material, 3d material, fibrils, ultimate strain | |
Estimating Thermal Decomposition Parameters for Lithium Hydride in a High Temperature Gas Flow
| Authors: Tovstonog V.A. | Published: 14.06.2018 |
| Published in issue: #3(120)/2018 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: lithium hydride, high temperature gas flow, heat-absorbing material, thermal decomposition, ablation, decomposition parameters | |
Soluton Algorthim of Generalized Non-Stationary Heat Conduction Problem in the Bodies of Simple Geometric Shapes
| Authors: Eliseev V.N., Tovstonog V.A., Borovkova T.V. | Published: 14.02.2017 |
| Published in issue: #1(112)/2017 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: temperature field, generalized heat conduction problem, bodies of a simple shape, solution algorithm | |
Mathematical Modeling of Solar Panel Temperature Dynamics in Various Conditions of Orbital Space Missions
| Authors: Astakhov N.N., Kargy D.L., Gorbulin V.I., Steganov G.B., Shubin D.A. | Published: 06.12.2016 |
| Published in issue: #6(111)/2016 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: solar light flux, reflected flux, albedo of the Earth, the temperature regime of the spacecraft, the terminator line | |