Computing aerodynamic properties for a model of a detachable fairing flap at a supersonic incident flow velocity
| Authors: Slobodyanyuk D.M. | Published: 26.04.2017 |
| Published in issue: #5(10)/2017 | |
| DOI: DOI: 10.18698/2541-8009-2017-5-101 | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
| Keywords: aerodynamic properties, SolidWorks software package, ANSYS software package, thin-walled shells, detachable parts, flow modeling | |
Numerical modeling of aerodynamic wind tunnel experiment
| Authors: Marashan М.V. | Published: 14.03.2017 |
| Published in issue: #5(5)/2016 | |
| DOI: DOI: 10.18698/2541-8009-2016-5-46 | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
| Keywords: aerodynamic experiment, wind tunnel, numerical simulation, Solid Works Flow Simulation | |
Employing a tether system for a Mars mission
| Authors: Birev N.V. | Published: 02.12.2016 |
| Published in issue: #3(3)/2016 | |
| DOI: DOI: 10.18698/2541-8009-2016-3-22 | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
| Keywords: tether system, spacecraft, orbit, tethered platform, delta-v, linear velocity, angular velocity, elliptical orbital velocity | |
Comparison of hypersonic aircraft quasi horizontal maneuver control methods
| Authors: Kalinovskiy T.A. | Published: 06.09.2016 |
| Published in issue: #1(1)/2016 | |
| DOI: DOI: 10.18698/2541-8009-2016-1-10 | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
| Keywords: hypersonic aircraft, control method, maneuvering, banking angle, atmosphere, optimal control | |