Investigating Interaction Intensity between Condensed Phase Particles and Flow Duct Components of a Small-Scale Ramjet
Authors: Voronetskiy A.V., Smolyaga V.I., Aref'ev K.Yu., Filimonov L.A., Abramov M.A. | Published: 02.08.2018 |
Published in issue: #4(121)/2018 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts | |
Keywords: mathematical simulation, two-phase flow, condensed particles, erosion, ramjet |
Estimating the Thermal State of a Screen Acting as Protection from Radiation Emitted by a Hot Gas Jet
Authors: Eliseev V.N., Babarykin E.I. | Published: 02.08.2018 |
Published in issue: #4(121)/2018 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aerodynamics and Heat Transfer Processes in Aircrafts | |
Keywords: screen, protection, radiation, thermal state, gas, insulation, structure |
Thermal Loading Simulators with Diffuse Emitter Modules Operating over a Strictly Bounded Solid Angle
Authors: Kolesnikov A.V., Paleshkin A.V., Shemetova E.V. | Published: 02.08.2018 |
Published in issue: #4(121)/2018 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircrafts Development, Design and Manufacture | |
Keywords: simulation, thermal loading, spacecraft, radiation phase function, diffuse radiation |
Performance of a Solar Thermal Propulsion Featuring Latent Heat Storage and Subsequent Hydrogen Burning
Authors: Finogenov S.L., Kolomentsev A.I. | Published: 02.08.2018 |
Published in issue: #4(121)/2018 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Innovation Technologies of Aerospace Engineering | |
Keywords: solar thermal propulsion, latent heat storage, phase-change materials, subsequent hydrogen burning, spacecraft, geostationary orbit |
Mathematical Simulation for Computing Process Parameters During Non-Steady-State Heating of Heat Exchanger Walls
Authors: Aleksandrov V.Yu., Koroleva A.P., Kukshinov N.V., Safonova D.B., Frantsuzov M.S. | Published: 02.10.2018 |
Published in issue: #5(122)/2018 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aerodynamics and Heat Transfer Processes in Aircrafts | |
Keywords: non-steady-state heat transfer, heat exchanger, mathematical simulation |
Determining Aerodynamic Loads Affecting an Aircraft Wing During Parametric Modelling Taking the Main Airliner Components into Account
Authors: Mikhaylovskiy K.V., Baranovski S.V. | Published: 02.10.2018 |
Published in issue: #5(122)/2018 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircrafts Development, Design and Manufacture | |
Keywords: airliner, wing, wing configuration, engine, aerodynamic loads, parametric simulation |
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 |
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 |
Thermal Mode of Sapphire Shells and Depth of Modulation of Radiation of Pulsed-Periodic Sources of Infrared Radiation
Authors: Gradov V.M., Gavrish S.V., Rudakov I.V. | Published: 17.02.2019 |
Published in issue: #1(124)/2019 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aerodynamics and Heat Transfer Processes in Aircrafts | |
Keywords: radiation source shell, temperature field, modulation depth, peak radiation power, discharge, infrared, simulation, spectra |
Development of a Launch Vehicle Control Algorithm at the Initial Flight Part in Case of one of the Engines
Authors: Trifonov M.V., Altshuler A.Sh., Bobronnikov V.T. | Published: 17.02.2019 |
Published in issue: #1(124)/2019 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
Keywords: launch vehicle, launch complex safety, engine failure, emergency displacement, optimal regulator, quadratic criterion |