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All Journal TEKNIK Jurnal Sains dan Teknologi Jurnal Simetris Jurnal Teknologi FLYWHEEL : Jurnal Teknik Mesin Untirta Teknika: Jurnal Sains dan Teknologi Jurnal Mechanical Media Mesin: Majalah Teknik Mesin R.E.M (Rekyasa Energi Manufaktur) Jurnal Jurnal Rekayasa Mesin Dinamika Teknik Mesin JOURNAL OF MECHANICAL ENGINEERING, MANUFACTURES, MATERIALS AND ENERGY JTM-ITI (Jurnal Teknik Mesin ITI) Machine : Jurnal Teknik Mesin Turbulen : Jurnal Teknik Mesin Angkasa: Jurnal Ilmiah Bidang Teknologi Journal Technology and Implementation Bussines Jurnal Elemen Manutech : Jurnal Teknologi Manufaktur JURNAL CRANKSHAFT Jurnal Muara Sains, Teknologi, Kedokteran dan Ilmu Kesehatan Jurnal Teknik Mesin Indonesia Infotekmesin Jurnal Energi dan Teknologi Manufaktur (JETM) Jurnal Mesin Nusantara Journal of Mechanical Engineering Internet of Things and Artificial Intelligence Journal Jurnal Teknologi dan Terapan Bisnis Jurnal Polimesin
Lasinta Ari Nendra Wibawa
Badan Riset dan Inovasi Nasional (BRIN)
Aerospace Engineering Automotive Engineering Chemical Engineering, Chemistry & Bioengineering Civil Engineering, Building, Construction & Architecture Computer Science & IT Control & Systems Engineering Decision Sciences, Operations Research & Management Education Electrical & Electronics Engineering Energy Engineering Industrial & Manufacturing Engineering Materials Science & Nanotechnology Mechanical Engineering Physics Transportation

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Journal : FLYWHEEL : Jurnal Teknik Mesin Untirta

 1 
PENGARUH SUSUNAN DAN JUMLAH LUBANG BAUT TERHADAP KEKUATAN RANGKA MAIN LANDING GEAR UNTUK PESAWAT UAV Lasinta Ari Nendra Wibawa
FLYWHEEL : Jurnal Teknik Mesin Untirta Volume V Nomor 1, April 2019
Publisher : Universitas Sultan Ageng Tirtayasa

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.36055/fwl.v0i0.4928

Abstract

This study examined the effect of the arrangement and number of bolt holes on the strength of the main landing gear frame for UAV aircraft using the finite element method. Linear static analysis was carried out using Autodesk Inventor Professional 2017 software. Main landing gear frame using Aluminum alloy 5083. Variable arrangement and number of bolt holes were 3 bolts (series), 3 bolts (zigzags), 4 bolts (series), 4 bolts (zigzags) ), 5 bolts (series), and 5 bolts (zigzags). The simulation results show that the safety factor is for the arrangement and the number of bolts 3 bolts (series), 3 bolts (zigzags), 4 bolts (series), 4 bolts (zigzags), 5 bolts (series), and 5 bolts (zigzags) were 3.498, 3.325, 3.843, 3.793, 3.401, and 3.338. 
Co-Authors Abdilah Hasan Hasan Adi Farmasiantoro Farmasiantoro Alit Daryana Asep Diana Diyat Muhdiyat Muhdiyat Dwi Aries Himawanto Dwi Aries Himawanto Gatot Suharto Abdul Fatah Handriyana Handriyana Iyus Rusyana Rusyana Jihad, Bagus H. Kukuh Yudistiro Kuncoro Diharjo Kuncoro Diharjo Parid Saparudin Rahadyan Lingga Laksita Toris Sobirin Tuswan Tuswan Unggul Satrio Yudhotomo Unggul Satrio Yudhotomo Wan Dedy Fitrah Indrayana Wijang Wisnu Raharjo Yopiek Kristiyana Kristiyana Yudi Haryanto Yudi Prastiyono