NUMERICAL ANALYSIS OF THE IMPACT OF SIDESLIP ANGLE ON LOAD OF THE GYROCOPTER STABILIZERS
Keyword(s):
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.
2019 ◽
Vol 233
(14)
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pp. 3621-3629
2020 ◽
2016 ◽
Vol 138
(9)
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2008 ◽
Vol 222
(4)
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pp. 183-192
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2019 ◽
Vol 10
(2)
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pp. 1072
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2010 ◽
Vol 29-32
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pp. 89-94
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2016 ◽
Vol 95
(9)
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pp. E9-E14
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