Features of Designing and Numerical Simulation of Flow Stabilizers in Actuator Line Synchronization Systems
| Authors: Ivanov M.Yu., Novikov A.E., Resh G.F. | Published: 12.04.2017 |
| Published in issue: #2(113)/2017 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircrafts Development, Design and Manufacture | |
| Keywords: line synchronizing system, flow stabilizer, spool-and-sleeve, hydrodynamic force, mathematical modeling, universal testbed for flow stabilizer testing, static characteristic | |
Nonisothermal Concentrator-Absorber System Performances for Solar Thermal Propulsion
| Authors: Finogenov S.L., Kolomentsev A.I. | Published: 12.04.2017 |
| Published in issue: #2(113)/2017 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts | |
| Keywords: solar thermal propulsion, concentrator-absorber system, nonisothermal heating, solar high-tempe-rature source of heat, geostationary orbit, upper stage | |
Computational and Experimental Research of the High-Speed Gas Flow Structure Near Aircraft Fragments Models
| Authors: Kotov M.A., Ruleva L.B., Solodovnikov S.I., Surzhikov S.T. | Published: 26.05.2017 |
| Published in issue: #3(114)/2017 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aerodynamics and Heat Transfer Processes in Aircrafts | |
| Keywords: shock aerodynamic tube, aerothermodynamics, computational and experimental research, shock-wave interaction, aircraft fragments models | |
Spark and Heated Surface Ignition Mechanism Effect on Launch of the Oxygen-Hydrogen Thruster
| Authors: Kochanov A.V., Klimenko A.G., Rebrov S.G. | Published: 26.05.2017 |
| Published in issue: #3(114)/2017 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts | |
| Keywords: thruster, ignition, glow plug, oxygen, hydrogen, combustion chamber, precombustion chamber | |
Influence of Heat Exchange Intensity in the Rocket Thrust Chamber on the Cooling Channel Efficiency
| Authors: Aleksandrenkov V.P. | Published: 03.08.2017 |
| Published in issue: #4(115)/2017 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts | |
| Keywords: annular channel, intensification of convective heat transfer, thermal and hydraulic efficiency and characteristics, maximum heat dissipation, heat transfer coefficients ratio, limiting efficiency | |
Research of Solid Hydrocarbon Fuel Gasification Products Mixing with High-Enthalpy Gas Flux in Uniform Cross-Section Ducts
| Authors: Fedotova K.V., Aref'ev K.Yu., Sukhov A.V., Yanovsky L.S. | Published: 03.08.2017 |
| Published in issue: #4(115)/2017 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts | |
| Keywords: numerical simulation, gas fluxes mixing, gasification products of solid hydrocarbon fuel, CFD, semiempirical turbulence model, pressure pulsations in supersonic gas jet | |
Thermodynamic Estimation of Fuel Efficiency for a High-Speed Ramjet Running on Hydrocarbon Fuel with Boron and Beryllium Hydride Additives
| Authors: Kruchkov S.V., Saveliev A.M. | Published: 14.09.2017 |
| Published in issue: #5(116)/2017 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts | |
| Keywords: fuel efficiency, hydrocarbon fuel, high-energy additives, thermodynamic estimation, high-speed ramjet | |
A Similarity Solution to the Heat Transfer Problem for an Isotropic Half-Space Featuring a Film-Coated Moving Boundary
| Authors: Attetkov A.V., Vlasov P.A., Volkov I.K. | Published: 14.09.2017 |
| Published in issue: #5(116)/2017 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aerodynamics and Heat Transfer Processes in Aircrafts | |
| Keywords: thermally thin coating, unsteady heat transfer, temperature field, similarity solution, isotropic half-space with a moving boundary | |
Оn Oscillations of a Semi-Cylinder Having a Cylindrical Cavity with Immiscible Liquids
| Authors: Win Ko Ko | Published: 05.12.2017 |
| Published in issue: #6(117)/2017 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircrafts Development, Design and Manufacture | |
| Keywords: stability, orbital refueling station, space tanker, cryogenic liquid, immiscible liquids, reduced masses | |
Temperature State of the Layer of Translucent Material with Depending on Temperature Thermal Conductivity and Absorption of Penetrating Radiation
| Authors: Zarubin V.S., Kuvyrkin G.N., Savelieva I.Yu. | 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: penetrating radiation, volumetric energy deposition, variation form of mathematical model, stationary point of the functional | |