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 |
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 |
Analysing Specifics of Manufacturing Items out of Polymer Composite Materials by Means of Filament Winding. Shaping Mandrels
Authors: Zuev A.S., Emashev A.Yu., Shaydurova G.I.  | Published: 14.06.2018 |
Published in issue: #3(120)/2018 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircrafts Development, Design and Manufacture | |
Keywords: filament winding, reinforcement, matrix, mandrel, deformation, heat setting |
Optimization of Hybrid Composite Material Structure for Wing Skin of Tourist Class Reusable Space Vehicle
Authors: Ageeva T.G., Ashikhmina E.R., Prosuntsov P.V. | Published: 09.02.2018 |
Published in issue: #1(118)/2018 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircrafts Development, Design and Manufacture | |
Keywords: reusable space vehicles, space tourism, hybrid polymer composite materials, wing |
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 |
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 |
Some Aspects of Small Spaceсraft Thermal-Vacuum Testing
Authors: Mayorova V.I., Mullin N.A. | Published: 12.04.2017 |
Published in issue: #2(113)/2017 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircrafts Development, Design and Manufacture | |
Keywords: small spacecraft, test methods, accelerated test, thermal vacuum tests, thermal model |
Feasibility Assessment of Thermally Stabilizing the Photodetector for Earth Remote Sensing with Thermoelectrical Cooler
Authors: Morozov A.S., Krotov A.S., Kas | Published: 19.10.2016 |
Published in issue: #5(110)/2016 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircrafts Development, Design and Manufacture | |
Keywords: photodetector, thermoelectrical cooler, passive thermal control system, cryogenic thermal storage unit, earth remote sensing |
Modeling of the Kinetics of Impregnation Process in the Production of Reinforced Carbon-Fiber Reflectors for Space Antennas
Authors: Pyi Phyo Maung, Malysheva G.V. | Published: 19.10.2016 |
Published in issue: #5(110)/2016 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircrafts Development, Design and Manufacture | |
Keywords: vacuum infusion, impregnation time, grid angle, reflector, modeling |
Discharge and Non-Dimensional Parameters of Fluid Flows in Throttles of Spool Hydraulic Valves of Electro Hydraulic Amplifiers
Authors: Belonogov O.B. | Published: 19.10.2016 |
Published in issue: #5(110)/2016 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircrafts Development, Design and Manufacture | |
Keywords: electro hydraulic amplifiers, spool hydraulic valves, identification method, non-dimensional parameter, fluid flow |