Multiple Regression for UAV Aerodynamic Model based on Experimental Data
| Authors: Koryanov V.V. , Nguyen K.T., Nguyen V.T. | Published: 19.10.2016 |
| Published in issue: #5(110)/2016 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
| Keywords: multiple regression, statistical synthesis, aerodynamic model, structural and parametric selection criterion, Unmanned Aerial Vehicle (UAV), correlation | |
Mathematical Modeling of Solar Panel Temperature Dynamics in Various Conditions of Orbital Space Missions
| Authors: Astakhov N.N., Kargy D.L., Gorbulin V.I., Steganov G.B., Shubin D.A. | Published: 06.12.2016 |
| Published in issue: #6(111)/2016 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: solar light flux, reflected flux, albedo of the Earth, the temperature regime of the spacecraft, the terminator line | |
Modeling of Heat Transfer in Decomposable Materials of Thermal Protection Coating of Reentry Vehicle
| Authors: Barinov D.Ya., Prosuntsov P.V. | Published: 06.12.2016 |
| Published in issue: #6(111)/2016 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aerodynamics and Heat Transfer Processes in Aircrafts | |
| Keywords: mathematical model, reentry, vehicle, thermal protection, decomposable material, ablation | |
Innovative Model of Liquid Nitrogen Application for Cooling Rocket Fuel Tanks Filling the Ground-Based Systems
| Authors: Aleksandrov A.A., Barmin I.V., Denisova K.I., Chugunkov V.V. | Published: 06.12.2016 |
| Published in issue: #3(114)/2017 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Ground Complexes, Launch Equipment, Aircraft Exploitation | |
| Keywords: rocket fuel, temperature preparation, tank storage, cooling, heat exchanger, antifreeze, liquid nitrogen | |
RANS Methods in Flow Problems of High Speed Aircraft Constructions Elements and Aircraft Engines for Features Analysis of Convective Heat Fluxes Numerical Simulation
| Authors: Voronetskiy A.V., Aref'ev K.Yu., Gusev A.A. | Published: 14.02.2017 |
| Published in issue: #1(112)/2017 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aerodynamics and Heat Transfer Processes in Aircrafts | |
| Keywords: mathematical modeling, convective heat transfer, axisymmetric channel, plate, de Laval nozzle, accuracy of calculation | |
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 | |
Dynamic of Emergency Fairing Separation from Launch Vehicle in Atmospheric Ascent
| Authors: Kokushkin V.V., Khomyakov M.K., Ovsyannikova N.Yu., Bogomolov N.V. | Published: 12.04.2017 |
| Published in issue: #2(113)/2017 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aerodynamics and Heat Transfer Processes in Aircrafts | |
| Keywords: separate fairing, emergency separation, separation dynamics, relative motion, stability rating | |
Spacecraft External Heat Flow Analysis by z-Buffer Method
| Authors: Soluyanov A.A. | Published: 12.04.2017 |
| Published in issue: #2(113)/2017 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aerodynamics and Heat Transfer Processes in Aircrafts | |
| Keywords: spacecraft, meshed geometrical model, mutual shading, pixel, z-buffer, depth buffer | |
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 | |
Investigation of Antipulsation Partitions Influence on the Working Process Development in Oxygen-Kerosene LRE Combustion Chamber with Jet-Centrifugal Injectors by Numerical Simulation
| Authors: Mosolov S.V., Sidlerov D.A. | 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: liquid rocket engine, combustion chamber, numerical simulation, fuel burning | |