Keywords
Very Light Aircraft (VLA)
aerial spray
Design Organization Approval (DOA)
European Aviation Safety Agency (EASA)
normativity
finite element simulation Aeronave Ultra Liviana (AUL)
aspersión área
Aprobación de Organización de Diseño (DOA)
Normatividad Agencia Europea de Seguridad aérea (EASA)
simulación por elementos finitos
aerial spray
Design Organization Approval (DOA)
European Aviation Safety Agency (EASA)
normativity
finite element simulation Aeronave Ultra Liviana (AUL)
aspersión área
Aprobación de Organización de Diseño (DOA)
Normatividad Agencia Europea de Seguridad aérea (EASA)
simulación por elementos finitos
How to Cite
Rios-Chaparro, C., Quintero-Arboleda, B., Ortega, I. ., Jaramillo-Suárez, H. ., & G., Z. (2022). Design, construction, and validation of structural components of a VLA category light aircraft for use in aerial spraying. Informador Tecnico, 86(2), 171–193. https://doi.org/10.23850/22565035.3943
Abstract
This paper presents the calculation, design, simulation, and validation of structural components of the light aircraft prototype CVAC-001 category VLA for use in aerial spraying. The regulation established by the EASA-ADOA (Alternative Design Organization Approval) was defined in the project as an aircraft design model to achieve its guarantee or assurance. For the calculation, design, simulation, and validation process of the structural components, two sides of the load frame and the set of three components that make it up were chosen. The finite element simulation for the static study of stress and buckling and the validation tests of the load frame allows us to conclude that the design feasibility criterion is met for the analyzed components.
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This work is licensed under a Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License.
Copyright (c) 2022 Servicio Nacional de Aprendizaje SENA
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