Numerical analysis of the impact of sideslip angle on load of the gyrocopter stabilizers
Autor: | Zbigniew Czyż, Paweł Karpiński |
---|---|
Jazyk: | angličtina |
Rok vydání: | 2020 |
Předmět: | |
Zdroj: | Aviation, Vol 23, Iss 4 (2020) |
Druh dokumentu: | article |
ISSN: | 1648-7788 1822-4180 |
DOI: | 10.3846/aviation.2019.11924 |
Popis: | The paper presents some of the works related to the project of modern gyrocopter construction with the possibility of a short start, known as "jump-start". It also presents a methodology related to numerical calculations using Computational Fluid Dynamics based on ANSYS Fluent three-dimensional solver. The purpose of the work was to calculate the forces and aerodynamic moments acting on the gyrocopter stabilizers. The calculations were carried out for a range of angle of attack α from –20° to +25° and for a sideslip angle β from 0° to 20°. Based on the calculations carried out, analysis of the impact of the slip angle on the load on the stabilizers has been made. First published online 17 February 2020 |
Databáze: | Directory of Open Access Journals |
Externí odkaz: |