All articles by "Tovstonog V.A."
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 |
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 |
Estimating the Thermal State of a Blunted Wedge in a High-Velocity Gas Flow
Authors: Zinin K.М., Aliev Az.A., Tovstonog V.A. | Published: 20.07.2019 |
Published in issue: #3(126)/2019 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aerodynamics and Heat Transfer Processes in Aircrafts | |
Keywords: high-velocity aircraft, aero-dynamic heating, thermal protection, refractory oxide materials, thermal state |
Evaluating the Potential of Lithium Hydride in Active Thermal Protection Systems for High-Velocity Aircraft
Authors: Tovstonog V.A. | Published: 22.04.2019 |
Published in issue: #2(125)/2019 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aerodynamics and Heat Transfer Processes in Aircrafts | |
Keywords: high-velocity aircraft, active thermal protection, phase-change materials, lithium hydride, linear pyrolysis |
Heat Transfer in a Flattened Pipe with an Ablative Wall
Authors: Tovstonog V.A. | Published: 07.12.2018 |
Published in issue: #6(123)/2018 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aerodynamics and Heat Transfer Processes in Aircrafts | |
Keywords: thermal protection, ablative material, lithium hydride, thermochemical decomposition, flattened pipe, heat transfer by radiation and convection |
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 |
Radiation Heat Transfer and Thermal Protection of Air-Gas Channel of Gas Dynamic Plant
Authors: Tovstonog V.A. | Published: 05.12.2017 |
Published in issue: #6(117)/2017 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aerodynamics and Heat Transfer Processes in Aircrafts | |
Keywords: gas dynamic installation, high temperatures, radiation heat transfer, thermal protection |
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 |