Wind Tunnel Aerodynamic Study of a VTOL-UAV for Wide Range of Angles of Attack and Sideslip Angles

Prieto, Victoria M.; Esteban, Sergio

doi:10.1007/s42496-020-00070-2

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Uav With Fixed Wings Aerodynamics1

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2022

2024

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Cited by 4 publications

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“…Aerodynamic forces and moments are determined based on the geometry of the aircraft using tables, simulations, and wind tunnel experiments [9]. To create a mathematical model, it is necessary to know the distribution of pressure coefficients around the aircraft.…”

Section: Uav With Fixed Wings Aerodynamicsmentioning

confidence: 99%

Verification of Selected Model Coefficients for a Small Unmanned Aircraft

Hlinková¹,

Andoga²,

Karaffa³

2022

Acta Avionica

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This article presents design and analysis of mathematical model UAV with fixed wings. The mathematical model serves to understand the basic mathematical principle and physical laws, that are applied to the system, and is indispensable in UAV movement simulation and modelling of the control algorithms. The article also describes the methodology of individual modelled parts using the XFLR5, where effective numerical methods are used for mathematical modelling. The last part provides verified and reliable results obtained by simulations of a mathematical model, which will be used to simulate basic and critical situation states.

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Section: Uav With Fixed Wings Aerodynamicsmentioning

confidence: 99%