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Analysis of the Aerodynamics Parameters and Design of the Fixed Wing for the Drone
The capacity of a wing to generate lift force is determined by the lift and drag coefficients produced by the effects of the airflow path along the selected airfoil and surface geometry. On this research, a methodology has been developed, based on the System Life Cycle management tool and mathematic...
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Published in: | International research journal of innovations in engineering and technology 2021-04, Vol.5 (4), p.87 |
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Main Authors: | , , , , |
Format: | Article |
Language: | English |
Subjects: | |
Online Access: | Get full text |
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Summary: | The capacity of a wing to generate lift force is determined by the lift and drag coefficients produced by the effects of the airflow path along the selected airfoil and surface geometry. On this research, a methodology has been developed, based on the System Life Cycle management tool and mathematical models to perform a theoretical, computational, and experimental aerodynamic analysis in order to design and model a fixed wing for an UAV. |
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ISSN: | 2581-3048 |
DOI: | 10.47001/IRJIET/2021.504014 |