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 | |
Influence of the Soil and Rocky Target Strength Properties on Projectiles Penetration Depth with Additional Action of the Jet Thrust Impulse
| Authors: Fedorov S.V., Fedorova N.A. | Published: 11.08.2016 |
| Published in issue: #4(109)/2016 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: high-velocity penetration, non-deformable projectile, soil and rocky target, strength properties, penetration depth, jet impulse, Tsiolkovsky number | |
Research on thermal conditions of a small space vehicle
| Authors: Sudomoin P.D., Shabanov V.A., Platonov K.A., Kas | Published: 29.03.2016 |
| Published in issue: #2(107)/2016 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: space vehicle, thermal mathematical model, concentrated parameters, passive control system, orbit thermal loads | |