Article Per Year (5 Year)
p-Index From 2019 - 2024
4.757
P-Index
This Author published in this journals
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

Published : 40 Documents Claim Missing Document
Claim Missing Document
Check
Articles

Found 40 Documents
Search

 1   2   3   4 
DESAIN DAN ANALISIS KEKUATAN RANGKA LEMARI PERKAKAS DI BALAI LAPAN GARUT MENGGUNAKAN METODE ELEMEN HINGGA Lasinta Ari Nendra Wibawa
Machine : Jurnal Teknik Mesin Vol 5 No 2 (2019): Machine : Jurnal Teknik Mesin
Publisher : Jurusan Teknik Mesin Fakultas Teknik Universitas Bangka Belitung

Show Abstract | Download Original | Original Source | Check in Google Scholar | Full PDF (456.676 KB) | DOI: 10.33019/jm.v5i2.787

Abstract

Penelitian ini mengkaji tentang perancangan dan analisis kekuatan rangka lemari perkakas menggunakan metode elemen hingga. Lemari perkakas didesain lima tingkat dengan ukuran 800 mm (panjang), 400 mm (lebar), dan 1750 mm (tinggi). Analisis dilakukan menggunakan software Autodesk Inventor Professional 2017. Material rangka yang digunakan adalah Aluminum paduan 3003-H12 dengan standar DIN EN 10056-1 (Equal angles) dengan ukuran 25 x 25 x 3 mm. Variabel beban tiap tingkat lemari perkakas yaitu 45 kg, 50 kg, 55 kg, dan 60 kg. Hasil simulasi menunjukkan untuk beban lemari perkakas tiap tingkat dengan berat 45 kg, 50 kg, 55 kg, dan 60 kg memiliki faktor keamanan berturut-turut yaitu 2,49, 2,24, 2,04, dan 1,87.
PENGARUH BEBAN TERHADAP PREDIKSI UMUR FATIK DUDUKAN (BRACKET) AC OUTDOOR MENGGUNAKAN METODE ELEMEN HINGGA LASINTA ARI NENDRA WIBAWA
JURNAL CRANKSHAFT Vol 3, No 1 (2020): Jurnal Crankshaft Vol.3 No.1 Maret 2020
Publisher : Universitas Muria Kudus

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.24176/crankshaft.v3i1.4320

Abstract

The study examines the effect of the load on fatigue life prediction of an outdoor AC bracket using the finite element method. Outdoor AC bracket design uses Autodesk Inventor Professional 2017, while finite element analysis uses Ansys Workbench. The outdoor AC bracket is subjected to a load of 20, 25, 30, and 35 kg with a fully-reserved type of loading. Gerber's mean stress theory is used to predict fatigue life. The outdoor AC bracket material uses Aluminum alloy 5052. The simulation results show that the outdoor AC bracket has a minimum fatigue life for loads of 20, 25, 30, and 35 kg, respectively is 1 x 108, 1.49 x 107, 1.93 x 106, and 6.64 x 105 cycles. Whereas the safety factor for minimum fatigue life for loads of 20, 25, 30, and 35 kg is 1.65; 1.32; 1.10; and 0.58. It shows the outdoor AC bracket can withstand the fatigue life of up to a minimum of 106 cycles for loads of 20, 25, and 30 kg because it has a safety factor of more than 1. While the 35 kg load of outdoor AC bracket fails to reach a minimum fatigue life of 106 cycles due to fatigue life prediction is only reached 6.64 x 105 cycles with a safety factor of less than 1, which is 0.58.
DESAIN DAN ANALISIS KEKUATAN DUDUKAN (BRACKET) AC OUTDOOR MENGGUNAKAN METODE ELEMEN HINGGA Lasinta Ari Nendra Wibawa
JURNAL CRANKSHAFT Vol 2, No 1 (2019): Jurnal Crankshaft Vol.2 No.1 Maret 2019
Publisher : Universitas Muria Kudus

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.24176/crankshaft.v2i1.2688

Abstract

Penelitian ini mengkaji tentang perancangan dan analisis kekuatan dudukan AC outdoor menggunakan metode elemen hingga. Analisis dilakukan menggunakan software Autodesk Inventor Professional 2017. Variabel beban AC outdoor yang diterima oleh masing-masing dudukan AC yaitu 156,96; 176,58; 196,2 , dan 215,82 N. Hasil simulasi menunjukkan untuk berat AC Outdoor 156,96; 176,58; 196,2, dan 215,82 N memiliki faktor keamanan berturut-turut yaitu 2,559; 2,275; 2,047, dan 1,861.
PENGARUH PEMILIHAN MATERIAL TERHADAP KEKUATAN RANGKA MAIN LANDING GEAR UNTUK PESAWAT UAV: EFFECT OF MATERIAL SELECTION ON THE STRENGTH OF THE MAIN LANDING GEAR FRAME FOR UAV AIRCRAF Lasinta Ari Nendra Wibawa
Jurnal Teknologi dan Terapan Bisnis Vol. 2 No. 1 (2019): Vol 2 No 1 (2019): Jurnal Teknologi dan Terapan Bisnis
Publisher : UPPM Akademi Komunitas Semen Indonesia

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.0301/jttb.v2i1.60

Abstract

This study examined the effect of material selection 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 5052-H38, Aluminium 5083 87 Cold Formed, Aluminium 6061, and CFRP. UAV aircraft was weighing 85 kg with a landing speed of 10 m/s and impact time of 0,5 second. The simulation results show that the landing gear frames of the lightest in a row were CFRP, Al 5083 87 Cold Formed, Al 5052-H38, and Al 6061. Materials that have the greatest safety factor were CFRP, Al 5083 87 Cold Formed, Al 6061, and Al 5052-H38.
Pengaruh Jumlah Ulir dan Variasi Beban terhadap Kekuatan Sambungan Cap dan Tabung Roket Dextrose Menggunakan Metode Elemen Hingga Lasinta Ari Nendra Wibawa; Adi Farmasiantoro Farmasiantoro; Abdilah Hasan Hasan; Diyat Muhdiyat Muhdiyat; Iyus Rusyana Rusyana; Yopiek Kristiyana Kristiyana; Unggul Satrio Yudhotomo
Journal of Mechanical Engineering Vol 5, No 2 (2021): Journal of Mechanical Engineering
Publisher : Universitas Tidar

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.31002/jom.v5i2.5277

Abstract

Kajian ini bertujuan untuk meneliti pengaruh jumlah ulir dan variasi beban terhadap kekuatan sambungan cap dan tabung roket Dextrose menggunakan metode elemen hingga. Cap dan tabung roket menggunakan Al 6063-T5. Ulir yang digunakan yaitu jenis ulir persegi dengan variasi jumlah ulir 5 dan 6 buah. Pembebanan divariasikan 4, 5, 6, dan 7 kN. Analisis elemen hingga dilakukan dengan bantuan software Ansys Workbench. Hasil simulasi tegangan statis menunjukkan semakin besar pembebanan, maka semakin tinggi tegangan von Mises maksimum. Tegangan von Mises maksimum menurun seiiring peningkatan jumlah ulir. Sambungan ulir persegi dengan variasi jumlah ulir 5 dan 6 dapat menahan beban statis hingga 6 kN karena memiliki faktor keamanan lebih dari 1,25.
Analisis Frekuensi Natural Rangka Main Landing Gear Pesawat UAV Menggunakan Ansys Workbench Lasinta Ari Nendra Wibawa
Jurnal Mesin Nusantara Vol 5 No 1 (2022): Jurnal Mesin Nusantara
Publisher : Universitas Nusantara PGRI Kediri

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.29407/jmn.v5i1.17580

Abstract

The main landing gear is one of the important components in UAV aircraft. This paper aims to analyze the natural frequency of the main landing gear and determine its normal mode shape. This analysis is important so that no resonance causes damage to the main landing gear components. The main landing gear uses Aluminum 6061 material and the analysis is carried out using the finite element method with the help of Ansys Workbench software. The analysis showed that the natural main landing gear frequencies for mode 1 to mode 6 were 76.04 Hz, 85.07 Hz, 167.82 Hz, 201.92 Hz, 288.39 Hz, and 327.00 Hz, respectively. The maximum deformation of the main landing gear for mode 1 to mode 6 is 33.73 mm, 35.35 mm, 48.16 mm, 44.62 mm, 38.14 mm, and 41.51 mm, respectively.
PENGARUH PEMILIHAN MATERIAL TERHADAP KEKUATAN RANGKA MAIN LANDING GEAR UNTUK PESAWAT UAV: EFFECT OF MATERIAL SELECTION ON THE STRENGTH OF THE MAIN LANDING GEAR FRAME FOR UAV AIRCRAF Lasinta Ari Nendra Wibawa
Jurnal Teknologi dan Terapan Bisnis Vol. 2 No. 1 (2019): Vol 2 No 1 (2019): Jurnal Teknologi dan Terapan Bisnis
Publisher : Program Studi Teknologi Informasi

Show Abstract | Download Original | Original Source | Check in Google Scholar | Full PDF (421.698 KB) | DOI: 10.0301/jttb.v2i1.60

Abstract

This study examined the effect of material selection 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 5052-H38, Aluminium 5083 87 Cold Formed, Aluminium 6061, and CFRP. UAV aircraft was weighing 85 kg with a landing speed of 10 m/s and impact time of 0,5 second. The simulation results show that the landing gear frames of the lightest in a row were CFRP, Al 5083 87 Cold Formed, Al 5052-H38, and Al 6061. Materials that have the greatest safety factor were CFRP, Al 5083 87 Cold Formed, Al 6061, and Al 5052-H38.
Detection of aflatoxin contamination in corn using The Simplified Gabor Wavelet algorithm Kukuh Yudistiro; Gatot Suharto Abdul Fatah; Lasinta Ari Nendra Wibawa; Yudi Prastiyono
Internet of Things and Artificial Intelligence Journal Vol. 3 No. 1 (2023): Vol. 3 No.1 (2023): Volume 3 Issue 1, 2023 [February]
Publisher : Association for Scientific Computing, Electronics, and Engineering (ASCEE)

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.31763/iota.v3i1.576

Abstract

The quality of corn is essential to determine whether the corn is still suitable for consumption and what type of corn it is. Corn is one type of vegetable that is indispensable for the nutritional needs of the Indonesian people today and is a mixture of other essential ingredients. Corn is rich in fiber, which is good for improving digestion and overcoming constipation, controlling blood sugar levels, maintaining heart health, overcoming depression, maintaining eye health, and preventing diverticulitis. In this research, image recognition is used to determine and detect the content of aflatoxin, which is one type of abnormality or disorder in corn. This affects the quality of corn, whether corn is suitable for human consumption, and what impact aflatoxin has on the human body. on testing using parameters Non UV image, SGW Filter Image θ = 0, 90, 180 and 270, and The resulting SGW image with the number of orientations N = 4, θ = θ + pi/N, and θ = θ + 2*pi/N, The aflatoxin content in humans can cause carcinogenic or liver cancer and acute necrosis, cirrhosis, and carcinoma in the animal liver.
Pengaruh diameter baut terhadap kekuatan rangka main landing gear pesawat UAV menggunakan metode elemen hingga Lasinta Ari Nendra Wibawa
Jurnal POLIMESIN Vol 17, No 1 (2019): Februari
Publisher : Politeknik Negeri Lhokseumawe

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.30811/jpl.v17i1.828

Abstract

Penelitian ini mengkaji tentang pengaruh diameter baut terhadap kekuatan rangka main landing gear untuk pesawat UAV menggunakan metode elemen hingga. Analisis statik linear dilakukan menggunakan software Autodesk Inventor Professional 2017. Material rangka main landing gear menggunakan Aluminium paduan 5083. Pesawat UAV memiliki berat 75 kg dengan kecepatan landing 10 m/s dan waktu impak 0,5 detik. Variabel diameter baut yaitu 11 mm, 12 mm, 13 mm, dan 14 mm. Hasil simulasi menunjukkan bahwa tegangan Von Mises untuk diameter baut 11 mm, 12 mm, 13 mm, dan 14 mm berturut-turut yaitu 82,092 MPa, 85,113 MPa, 85,141 MPa, dan 85,340 MPa. Nilai deformasi untuk diameter baut 11 mm, 12 mm, 13 mm, dan 14 mm berturut-turut yaitu 2,173 mm, 2,185 mm, 2,194 mm, dan 2,204 mm. Nilai faktor keamanan untuk diameter baut 11 mm, 12 mm, 13 mm, dan 14 mm berturut-turut yaitu 3,472, 3,349, 3,347, dan 3,340. Dari hasil simulasi dapat disimpulkan bahwa diameter baut terbaik adalah berukuran 11 mm. Kata kunci:  Aluminium 5083, Autodesk Inventor 2017, Analisis Elemen Hingga, Main Landing Gear, Diameter Baut AbstractThis study examined the effect of bolt diameter on the strength of the main landing gear frame for UAV aircraft using the finite element method. Linear static analysis was carried out using the Autodesk Inventor Professional 2017 software. Main landing gear frame using Aluminum alloy 5083. UAV aircraft weighed 75 kg with a landing speed of 10 m / s and an impact time of 0.5 seconds. Variables of bolt diameter were 11 mm, 12 mm, 13 mm and 14 mm. The simulation results show that Von Mises stress for bolt diameters 11 mm, 12 mm, 13 mm, and 14 mm were 82.092 MPa, 85.113 MPa, 85.141 MPa and 85.340 MPa respectively. Deformation values for bolt diameters of 11 mm, 12 mm, 13 mm, and 14 mm respectively were 2.173 mm, 2.185 mm, 2.194 mm and 2.204 mm. The safety factor values for bolt diameters were 11 mm, 12 mm, 13 mm, and 14 mm respectively, which are 3.472, 3.349, 3.347, and 3.340. From the simulation results it can be concluded that the best bolt diameter was 11 mm in size. Keywords: Aluminum 5083, Autodesk Inventor 2017, Finite Element Analysis, Main Landing Gear, Bolt Diameter 
Weight optimization of 200 mm diameter rocket motor tube using finite element method Lasinta Ari Nendra Wibawa; Alit Daryana; Parid Saparudin; Wan Dedy Fitrah Indrayana; Handriyana Handriyana; Asep Diana; Toris Sobirin
Jurnal POLIMESIN Vol 21, No 6 (2023): December
Publisher : Politeknik Negeri Lhokseumawe

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.30811/jpl.v21i6.4142

Abstract

The lightweight design of the rocket motor tube is a critical requirement for enhancing the rocket's flight performance. This study assesses the impact of wall thickness, cap thickness, and fillet radius on structural strength and the optimization of rocket motor tube weight using the finite element method with the assistance of Ansys software. A total of 12 finite element model variations, utilizing Aluminium 6061-T6, were developed and subjected to a uniform internal operating pressure load of 10 MPa. The design includes wall thickness variations of 8 and 10 mm, cap thickness options of 25 and 30 mm, and fillet radius dimensions of 20, 25, and 30 mm, allowing for a comprehensive comparison to achieve the required minimum safety factor while minimizing structural weight. The research concludes that increasing the fillet radius is a more recommended approach compared to increasing wall thickness and cap thickness. The results indicate that Model 9, with wall thickness, cap thickness, and fillet radius dimensions of 10 mm, 25 mm, and 30 mm, respectively, is the optimal choice due to its lightweight construction.
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