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Hasil Pencarian

Ditemukan 1 dokumen yang sesuai dengan query
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Muhammad Musyfiq Haikal
Numerical study of drag force on the uav tilt and fixed wing model during vertical take off landing
" A hybrid vertical take-off landing (VTOL) UAV combines the concepts of fixed-wing and rotary-wing UAV aircraft in one platform while performing in both conventional and vertical take-off landings. This aircraft has a drawback of significant drag force generated due to fixed-wing. Therefore, a Tilt-Wing often utilized to overcome this obstacle whereby it could be adjusted to the vertical and horizontal directions. To enhance the understanding of generated drag force on both wing model, this study ... "
Yogyakarta: Pusat Penelitian dan Pengabdian Pada Masyarakat (P3M) STTA, 2022
620 JIA XIV:1 (2022)
Artikel Jurnal  Universitas Indonesia Library