The influence of advance ratio on delta-winged uav vortex properties

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Détails bibliographiques
Auteur principal:	Santhoshinii Ramalingam
Autres auteurs:	Shabudin Mat, supervisor
Format:	Bachelor thesis
Langue:	anglais
Publié:	Universiti Teknologi Malaysia 2025
Sujets:	Mechanical engineering
Accès en ligne:	https://utmik.utm.my/handle/123456789/45348
Abstract	Abstract here

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