Perancangan dan analisis karakteristik aerodinamik pada pesawat fix wing VTOL UAV
نویسندگان
چکیده
Unmanned aerial vehicle (uav) merupakan wahana udara tanpa awak yang dikendalikan dari jarak jauh. Pemanfaatan ini salah satunya sebagai media pemantauan memiliki keunggulan pada nilai efektifitas kerjanya. Untuk melakukan pengamatan daerah perkotaan diperlukan rancangan pesawat uav dapat lepas landas dan mendarat secara vertikal (vtol) kecepatan tinggi dalam perpindahan satu tempat ke lainnya. Tahap pertama perancangan vtol adalah menentukan geometri sesuai kriteria telah ditentukan, kemudian dilakukan pemodelan analisis aerodinamik dengan menggunakan software solidwork . Hasil panjang fuselage 1,1849 meter, wing span 3 berat 5,9 kg. diperoleh CLmax sebesar 0,363125 sudut serang 4 o , CDmax 0,199722 efisiensi max 1,81815 0
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ژورنال
عنوان ژورنال: Angkasa
سال: 2023
ISSN: ['2581-1355', '2085-9503']
DOI: https://doi.org/10.28989/angkasa.v15i1.1373