Assessment of Anisotropy on Strength Properties of the Propulsion System Combustion Chamber Heat-Protective Coating During Changes in Ambient Temperature
| Authors: Ushakova E.S., Tuponogov V.G. | Published: 13.04.2026 |
| Published in issue: #1(156)/2026 | |
| DOI: | |
| Category: Power Engineering | Chapter: Theoretical and Applied Heat Engineering | |
| Keywords: solid-fuel rocket engine, combustion chamber heat-protective coating, nitrile butadiene rubber, calender effect, extrusion, thermocycling | |
Accounting for the Heater Inertiain the Single-Flow Non-Stationary Method to Study the Heat Transfer Surfaces
| Authors: Egorov K.S., Stepanova L.V. | Published: 12.01.2026 |
| Published in issue: #4(155)/2025 | |
| DOI: | |
| Category: Power Engineering | Chapter: Theoretical and Applied Heat Engineering | |
| Keywords: single-flow non-stationary method, maximum slope, heat transfer coefficient, heat transfer surface | |
A Model of the Coolant Transverse Thermal Conductivity Ideal Displacement in the Direct-Flow Plate Heat Exchangers
| Authors: Ryazhskikh A.V., Krasnov A.A., Ryazhskikh V.I. | Published: 23.01.2025 |
| Published in issue: #4(151)/2024 | |
| DOI: | |
| Category: Power Engineering | Chapter: Theoretical and Applied Heat Engineering | |
| Keywords: plate heat exchanger, direct flow, ideal displacement, laminar flow | |
Simulating Temperature State of Structures with the Power Elements using the Example of an Aircraft Fuel Compartment Exposed to Radiation Heating
| Authors: Gvozdev M.S., Lopukhov I.I. | Published: 24.07.2024 |
| Published in issue: #2(149)/2024 | |
| DOI: | |
| Category: Power Engineering | Chapter: Theoretical and Applied Heat Engineering | |
| Keywords: radiation heaters, aircraft, fuel compartment, reinforcement elements, combined method, thermal tests | |
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 | |
Convective Heat Exchange and Friction in a Thin Laminar-to-Turbulent Boundary Layer on the Impermeable Lateral Surfaces of Blunted Cones Featuring a Low Aspect Ratio
| Authors: Gorskiy V.V., Savvina A.G. | Published: 06.09.2021 |
| Published in issue: #3(138)/2021 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aerodynamics and Heat Transfer Processes in Aircrafts | |
| Keywords: convective heat transfer, friction, impulse loss thickness, boundary layer | |
Thermodynamic Rationale for Using Expander-Compressor Gas Turbine Power Unit
| Authors: Strebkov A.S., Osipov A.V., Zhavrotskiy S.V. | Published: 28.03.2021 |
| Published in issue: #1(136)/2021 | |
| DOI: | |
| Category: Power Engineering | Chapter: Heat Engines | |
| Keywords: тurbo-expander, gas turbine unit, thermodynamic cycle, the degree of pressure increase, specific fuel consumption, absolute thermal efficiency | |
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 | |
Simulating Heat Exchange and Friction in a Thin Laminar Boundary Layer of Air over the Lateral Surface of a Blunted Cone Featuring a Low Aspect Ratio
| Authors: Gorskiy V.V., Loktionova A.G. | Published: 18.12.2020 |
| Published in issue: #6(135)/2020 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aerodynamics and Heat Transfer Processes in Aircrafts | |
| Keywords: сonvective heat transfer, friction, impulse loss thickness, boundary layer | |
Modified Algebraical Cebeci --- Smith Turbulent Viscosity Model for the Entire Surface of a Blunted Cone
| Authors: Gorskiy V.V., Loktionova A.G. | Published: 11.08.2020 |
| Published in issue: #4(133)/2020 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aerodynamics and Heat Transfer Processes in Aircrafts | |
| Keywords: heat transfer, turbulence, boundary layer, effective length method | |