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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 | |