Longitudinal flight dynamics and stability of blended wing-body unmanned aerial vehicle with canard as control surface / Rizal Effendy Mohd Nasir

Blended wing-body (BWB) aircraft concept has its body ‘blended’ with the wing in smooth transition. Unlike conventional aircraft design, BWB aircraft’s body produces lift force and this causes large impact on the flight dynamics and stability. This thesis focuses on flight dynamics of a small unmann...

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Detalles Bibliográficos
Autor Principal: Mohd Nasir, Rizal Effendy
Formato: Thesis
Idioma:English
Publicado: 2013
Acceso en liña:https://ir.uitm.edu.my/id/eprint/16486/6/16486.pdf