CALCULATION OF THE AERODYNAMIC COEFFICIENTS USING MATLAB®
The article presents the calculation of aerodynamic coefficients of an airship wing's design: sustentation and moment coefficient applying two methods of integration. As a theoretical part, the fine theory of the aerodynamic profile is used and as a calculation tool the MATLAB software is used,...
| Autores: | , |
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| Tipo de recurso: | artículo |
| Estado: | Versión publicada |
| Fecha de publicación: | 2005 |
| País: | Perú |
| Institución: | Universidad Nacional Mayor de San Marcos |
| Repositorio: | Revistas - Universidad Nacional Mayor de San Marcos |
| Idioma: | español |
| OAI Identifier: | oai:revistasinvestigacion.unmsm.edu.pe:article/6167 |
| Acceso en línea: | https://revistasinvestigacion.unmsm.edu.pe/index.php/idata/article/view/6167 |
| Access Level: | acceso abierto |
| Palabra clave: | Aerodynamic profile Sustentation coefficient Incidence angle Attack angle Wind relative speed. Perfil aerodinámico Coeficiente de sustentación Ángulo de incidencia Ángulo de ataque Velocidad relativa del viento. |
| Sumario: | The article presents the calculation of aerodynamic coefficients of an airship wing's design: sustentation and moment coefficient applying two methods of integration. As a theoretical part, the fine theory of the aerodynamic profile is used and as a calculation tool the MATLAB software is used, through programs which are presented in their respective files. Besides, the outcome of results reports are presented. |
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