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All Journal Conference SENATIK STT Adisutjipto Yogyakarta
Lesalli, Prytha Virgiawan
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Aerospace Engineering Computer Science & IT Electrical & Electronics Engineering Industrial & Manufacturing Engineering Mechanical Engineering

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Longitudinal static stability analysis with wing swept angle variation of UAV flying wing surveillance adelaar 2 use software XFLR 5 Lesalli, Prytha Virgiawan; Cahyono, M. Ardi
SENATIK STT Adisutjipto Vol 6 (2020): Keselamatan Penerbangan di masa Pandemi Covid-19 [ISBN 978-602-52742-2-0]
Publisher : Institut Teknologi Dirgantara Adisutjipto

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.28989/senatik.v6i0.402

Abstract

Aircraft stability is very important  for calculated in aircraft design, specially for UAV which will be used for air surveillance. The purpose of aircraft stability analysis to find aircraft stability characteristic. Aircraft static stability can be analyzed by XFLR 5 Software which is can calculate characteristic of aircraft static stability, show visual, graph, and simulation of aircraft stability. Adellar 2 is UAV with flying wing configuration and will be analyzed use software XFLR 5 with the input of aircraft mass with the centre of gravity  wil be located in 5% of mean aerodynamic chord in front of neutral point and aircraft geometry types of airfoil in chord root, tip, span , winglet geometry and wing swept. With the result that Adelaar 2 is qualify for longitudinal static stability after the author analyze use XFLR5 with the parameter Cma<0  and obtained character of stability for 22.5o , 25o , 27.5o and 30o wing swept angle.
Preliminary Design dan Analisis Weight and Ballance Surveillance Mapping UAV Tricopter V-TOL Tilt Rottor 2 Meter Wing Span Lesalli, Prytha Virgiawan
SENATIK STT Adisutjipto Vol 7 (2022): Generation Z's Participation in Aerospace
Publisher : Institut Teknologi Dirgantara Adisutjipto

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.28989/senatik.v7i0.461

Abstract

Preliminary design merupakan langkah yang dilakukan untuk merancang pesawat udara, sebelum dilakukanya detail design dan analisis lebih lanjut. UAV (Unmanned Aerial Vehicle) Surveillance dan Mapping umumnya digunakan untuk memantau serta memetakan suatu wilayah dengan berbagai macam tujuan. Perancangan awal pesawat UAV ini dilakukan untuk menentukan wing loading, power weight ratio serta untuk mencari nilai luas sayap dan power motor yang diperlukan untuk menunjang UAV secara analitik yang menggunakan 3 motor dengan kemampuan take-off dan landing secara vertical serta motor dapat melakukan tilting supaya pesawat dapat melaju secara horizontal dengan kecepatan cruise 16 m/s dan kecepatan maksimal 24 m/s. Mencari nilai massa dan titik pusat massa airframe UAV dengan memasukan properti beberapa material berupa massa jenis pada komponen-komponen airframe menggunakan software CATIA V5, hasil analisis massa airframe menggunakan CATIA digabungkan dengan komponen-komponen UAV yang lain sehingga didapatkan massa total dan titik pusat massa UAV. Didapatkan massa total 6165 gr, luas sayap 0,575 m2, power requirement 395 W, serta pusat massa sebesar 141.183mm dibelakan leading edge chord root.
Co-Authors Cahyono, M. Ardi