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All Journal Journal of Dentistry Indonesia Rekayasa Mesin Automotive Experiences Recent in Engineering Science and Technology Prosiding SNTTM Indonesian Journal of Aerospace
Mohammad Adhitya, Mohammad
Department Of Mechanical Engineering Universitas Indonesia
Aerospace Engineering Agriculture, Biological Sciences & Forestry Astronomy Automotive Engineering Chemical Engineering, Chemistry & Bioengineering Control & Systems Engineering Dentistry Electrical & Electronics Engineering Energy Engineering Industrial & Manufacturing Engineering Materials Science & Nanotechnology Mechanical Engineering

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 1 
Comparison of Popular Three-Dimensional Printing Materials for Oral and Maxillofacial Surgical Guidance Model Adhitya, Mohammad; Sunarso, Sunarso; Muis, Abdul
Journal of Dentistry Indonesia Vol. 27, No. 3
Publisher : UI Scholars Hub

Show Abstract | Download Original | Original Source | Check in Google Scholar

Abstract

The application of three-dimensional (3D) models in the medical field has become popular. However, the accuracy of 3D models for surgical guidance varies among different materials and 3D printing technologies, such as printing machine usage. Objectives: This study aims to obtain more information about the effect of three different materials printed using a fused deposition material printer from the same digital data source. This study also aims to compare, analyze, and test the materials’ ability. Methods: Each of the filament materials (acetylbutane stearate [ABS], polylactic acid [PLA], and high-impact polystyrene [HIPS]) are printed at two infill densities, their weight, volume, and dimension are measured, and infill materials are prepared. Printing time is estimated and calculated on the basis of printing properties by using Simplify3D© software. The strength and surface tension of each sample are examined via a drilling test. Results: PLA is better than ABS and HIPS for printing our 3D model because of its properties. Conclusion: Ideal 3D materials for printing 3D models should fulfill the criteria on accuracy, strength, weight, and durability for usage. However, production time and cost should also be considered.
OPTIMIZATION OF LIGHTWEIGHT ELECTRIC BUS FRAME DESIGN THROUGH VALUE ENGINEERING APPROACH: A SYSTEMATIC REVIEW AND PARAMETRIC FEASIBILITY ANALYSIS Artana, I Nyoman; Sumarsono, Danardono Agus; Huda, Mahfudz Al; Adhitya, Mohammad
Jurnal Rekayasa Mesin Vol. 16 No. 2 (2025)
Publisher : Jurusan Teknik Mesin, Fakultas Teknik, Universitas Brawijaya

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.21776/jrm.v16i2.2119

Abstract

Lightweight frame design plays a critical role in improving the efficiency and sustainability of electric buses. This study aims to explore the optimization of electric bus frame design through the application of Value Engineering (VE), using a systematic literature review (SLR) supported by technical simulation references. The review focused on key parameters, including material selection, structural topology, component dimensions, and production costs, analyzed across more than 40 publications from reputable databases over the past decade. Various studies demonstrate that substituting conventional steel with aluminum alloy 6063 can reduce frame weight by up to 30%, while topology optimization based on Finite Element Analysis (FEA) achieves more efficient load distribution and structural integrity.  Additionally, shifting from manual to robotic welding methods has shown to enhance production efficiency by approximately 20%. Despite higher initial costs, VE supports long-term benefits by reducing operational costs, improving energy consumption, and aligning with sustainability goals. The findings suggest that integrating VE into the early stages of electric bus frame design offers a strategic pathway toward lighter, safer, and more cost-effective transportation solutions.
Experimental Stress Analysis on Frame Structure of A 70-Passengers Electric Bus Kristianto, Stevanus Brian; Adhitya, Mohammad; Haryanto, Budi; Deprian, Lukyawan Pama; Aziz, Umar Abdul; Dwimansyah, Ridho; Sumarsono, Danardono Agus
Automotive Experiences Vol 8 No 2 (2025)
Publisher : Automotive Laboratory of Universitas Muhammadiyah Magelang in collaboration with Association of Indonesian Vocational Educators (AIVE)

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.31603/ae.13757

Abstract

Structural strength testing of buses using static vertical load has not previously been explored to validate the structural integrity of bus frames. In this study, the static vertical load method was employed to validate the structural strength of the Universitas of Indonesia electric bus, which utilizes two different materials SS400 for the lower frame and Aluminum Alloy 6061 for the upper frame. Finite Element Analysis (FEA) was conducted to identify critical areas on both the lower and upper frames. The stress values in the simulation were also obtained at the same location as the strain gauge placements in the experiment. Experimental vertical load testing was carried out by incrementally applying a load of 1000 kg up to the equivalent of 70 passengers, with an additional dynamic coefficient of 30% resulting in a maximum load of 6850 kg. Strain measurements were taken using 20 strain gauges on the lower frame and 8 on the upper frame. The experimental result showed the highest stress occurred at strain gauge no. 9 on the lower frame, measuring 78.10 MPa, and 15.32 MPa on the upper frame under 6850 kg load. The comparison between the simulation and experimental results reveals an 18% deviation. Nevertheless, both methods indicate the same critical area of the structure. The stress distribution indicated that the central deck area of the lower frame, where passengers sit and stand, experienced the highest loads. On the upper frame, significant stress was observed in the area where the air conditioning system is mounted. These findings demonstrate that static vertical load testing can be effectively used to validate the structural strength and stress distribution of electric buses, particularly in areas subject to concentrated loading.
Effect of Hybridization on Tensile, Shear and Compressive Properties of Carbon Based Fiber Reinforced Composites Abdurohman, Kosim; Adhitya, Mohammad
Indonesian Journal of Aerospace Vol. 19 No. 2 (2021)
Publisher : BRIN Publishing

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.30536/j.jtd.2021.v19.a3575

Abstract

The high specific stiffness and strength of composites make them widely used  in defence, marine, and aerospace applications. Hybrid composites have increased use in high-tech applications. The glass/carbon and KC/carbon hybrid composites manufactured by vacuum assisted resin infusion methods are used in this study. The matrix used for both composites are vinylester resin. The glass/carbon and KC/carbon hybrid laminates arrangement is [G/C/G2/C/G2/C]s and [(KC)2/C3]s, respectively. The mechanical properties are evaluated according to ASTM standards. Fracture micrograph analysis are investigated using SEM. The comparison of mechanical properties and surface fracture of both hybrid composites have been investigated. The tensile and compressive strength of KC/carbon are higher than glass/carbon hybrid composites. However, the shear strength of KC/carbon is lower than glass/carbon hybrid composites. SEM micrograph exhibits that the KC/carbon has a good fiber/matrix and interlayer bond better than glass/carbon hybrid composites.
Analisis Kekuatan Struktur Komposit Dengan Ply Drop-off Pada Roda Pendarat Utama Pesawat Nir Awak Menggunakan Metode Elemen Hingga Wandono, Fajar Ari; Adhitya, Mohammad
Indonesian Journal of Aerospace Vol. 17 No. 1 Juni (2019): Jurnal Teknologi Dirgantara
Publisher : BRIN Publishing

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.30536/j.jtd.2019.v17.a3037

Abstract

Penggunaan ply drop-off telah banyak digunakan untuk mengoptimalkan struktur komposit sehingga memiliki massa yang lebih ringan dibandingkan dengan struktur komposit dengan penggunaan ketebalan seragam. Tulisan ini akan memprediksi kekuatan dan potensi pengurangan massa struktur komposit dengan menggunakan ply drop-off pada roda pendarat utama pesawat nir awak terhadap beban operasional menggunakan metode elemen hingga. Beban operasional diasumsikan merupakan beban statik akibat landing sebesar 245 N arah vertikal dan sebesar 78.75 N arah horizontal. Struktur roda pendarat utama dimodelkan menggunakan elemen Quad4 dengan memasukkan sifat mekanis dari material e-glass Woven Roving 185 pada software MSC. Patran/Nastran. Kriteria kegagalan yang digunakan adalah berdasarkan kriteria kegagalan Tsai-Wu dalam indeks kegagalan dan margin of safety. Hasil yang didapatkan adalah struktur roda pendarat utama memiliki indeks kegagalan 0.62 dan margin of safety sebesar 1.39. Dari hasil tersebut menandakan struktur roda pendarat utama cukup kuat dan tidak terjadi kegagalan dalam menerima beban operasional yang diberikan. Di samping itu, potensi pengurangan massa pada struktur roda pendarat utama menggunakan ply drop-off adalah sebesar 18%.
Technical and Economic Study of Fast Charging Systems Electric Heavy Equipment in Industrial and Port Areas Noval, Rahmat; Asep Apriana; Sumarsono, Danardono Agus; Dedi Junaedi; Fuad Zainuri; Mohammad Adhitya; Muhammad Hidayat Tullah; Fuzi Rachmat Ramdhan
Recent in Engineering Science and Technology Vol. 4 No. 01 (2026): RiESTech Volume 04 No. 01 Years 2026
Publisher : MBI

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.59511/riestech.v4i01.143

Abstract

The electrification of heavy equipment presents both an opportunity and a challenge for Indonesia’s industrial and port operations. Despite advancements in battery energy density and power electronics, the lack of efficient fast-charging infrastructure remains a critical bottleneck. This study evaluates the technical and economic feasibility of implementing high-power DC fast-charging systems for electric heavy machinery in port and industrial settings. Using HOMER Grid and MATLAB-based simulations, three charging configurations (90 kW AC, 250 kW DC, and 500 kW dual-gun DC) were analyzed. Results indicate that the 500 kW system reduces downtime by up to 70%, increasing equipment availability from 75% to 96%. Economic analysis shows a payback period of 4.8 years, internal rate of return (IRR) of 18.7%, and levelized cost of electricity (LCOE) of IDR 2,100/kWh. The findings support the deployment of modular fast-charging hubs to accelerate electrification in logistics and port sectors
Evaluasi keselamatan kebakaran kendaraan bermotor Nugroho, Yulianto Sulistyo; Nugroho, Reza Adyanto; Adhitya, Mohammad; Santoso, Muhammad Agung
Prosiding SNTTM Vol 23 No 1 (2025): SNTTM XXIII October 2025
Publisher : BKS-TM Indonesia

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.71452/qmde8743

Abstract

Risiko kebakaran kendaraan bermotor terus meningkat sejalan dengan meningkatnya populasi kendaraan bermotor serta mobilitas masyarakat. Kebakaran kendaraan bermotor dapat terjadi di perjalanan, di stasiun pengisian bahan bakar umum atau di dalam bangunan saat kendaraan di parkir. Kebakaran kendaraaan bermotor bukan saja menimbulkan kerusakan pada kendaraan, bangunan gedung parkir, tetapi juga dapat mengakibatkan cidera bahkan fatalitas penumpang kendaraan bermotor tersebut. Risiko kebakaran kendaraan bermotor baik berupa kendaraan dengan mesin pembakaran dalam (internal combustion engine - ICE) atau kendaraan listrik (electric vehicle – EV) ditandai dengan laju pelepasan kalor (heat release rate) akibat terbakarnya komponen / bahan mampu bakar yang ada di dalam kendaraan, maupun terbakarnya bahan bakar atau baterei sebagai sumber energi penggerak utama kendaraan bermotor. Untuk memberikan Gambaran mengenai risiko kebakaran kendaraan bermotor, makalah ini menyajikan metode pengukuran laju pelepasan kalor, kaji literatur hasil pengukuran eksperimental, dan evaluasi keselamatan kebakaran kendaraan bermotor sebagai upaya meningkatkan kepedulian dan keselamatan masyarakat pada umumnya.   
Optimizing the performance of gasoline-ethanol-methanol fueled engines with variations in the air-fuel ratio Mokhtar; Agus Sumarsomo, Danardono; Adika Agama, Askar; Adhitya, Mohammad
Prosiding SNTTM Vol 23 No 1 (2025): SNTTM XXIII October 2025
Publisher : BKS-TM Indonesia

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.71452/638pey73

Abstract

The 125 cc, four-stroke, air-cooled, electronic fuel injection SI engine for motorcycles was used to compare the effects of mixing methanol and ethanol with gasoline on engine power, fuel efficiency, and engine emissions. The test took place on the engine test bench. the fuel blending variation is 80% gasoline with various methanol-ethanol percentages. The result shows that The maximum torque value of all fuel mixture variants is achieved in the M20 mixture at λ= 0.9 at 6000 RPM, namely 8.52 Nm. The power value shows the highest value in the M20 mixture with λ= 1.1, namely 6.45 kW and the lowest value of SFC is 266.3 g/KWh obtained by the E10M10 mixture at 6000 RPM engine speed at λ=1.3
Tahapan Dalam Desain Konseptual Mobil terbang Bersayap Tetap Adhitya, Mohammad; Irwansyah, Ridho
Prosiding SNTTM Vol 23 No 1 (2025): SNTTM XXIII October 2025
Publisher : BKS-TM Indonesia

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.71452/y76aae85

Abstract

Mobil terbang adalah suatu wahana yang harus mampu beroperasi di jalan raya selayaknya mobil yang kita ketahui secara umum yang wajib memenuhi regulasi mobil raya meliputi dimensi dan hal-hal lain untuk memastikan keselamatan di jalan raya. Mobil terbang di sisi lain saat berfungsi sebagai pesawat terbang relatif tidak dibatasi dalam hal dimensi namun kinerjanya sangat dipengaruhi oleh aspek aerodinamika yang sangat dipengaruhi oleh perbandingan gaya angkat terhadap gaya berat pesawat (lift to weight ratio). Meskipun dinamakan sebagai mobil terbang, namun dari segi teknis dan tahapan desainnya, wahana ini lebih merupakan suatu pesawat terbang yang didesain sedemikian rupa agar dimensi serta sistem roda penopangnya dapat memenuhi fungsi dan regulasi dari suatu mobil. Dalam tulisan ini disampaikan suatu tahapan terstruktur dalam mendesain suatu mobil terbang yang merupakan kombinasi dari parameter-parameter penting suatu desain mobil dan pesawat terbang yang terdiri dari 8 tahapan yaitu 1. Requirements, 2. Weight estimation, 3. Critical performance parameters, 4. Configuration layout, 5. Force analysis due to CG position, 6. Better weight estimation, 7. Performance analysis, dan 8. Optimization. Hasil dari tahapan ini tentunya berupa desain mobil terbang yang dapat memenuhi fungsinya sebagai mobil yang memenuhi regulasi jalan raya dan sebagai pesawat terbang.
Co-Authors A. Azis Abdul Muis Abdurohman, Kosim Adika Agama, Askar Agus Sumarsomo, Danardono Ardian Roekettino Ardian Roekettino, Ardian Artana, I Nyoman Asep Apriana Bayu Trianto Bayu Trianto, Bayu Budi Haryanto D. A. Sumarsono Danardono Agus Sumarsono Dedi Junaedi Deprian, Lukyawan Pama Dwimansyah, Ridho F. A. Falah F. Arrafi F. Zainuri Fuad Zainuri fuzi rachmat ramdhan G. Fauzan Huda, Mahfudz Al I. Choiri I. Wahyudi Kristianto, Stevanus Brian M. Triananda Mokhtar Muhammad Hidayat Tullah Nandy Putra Noval, Rahmat Nugroho, Reza Adyanto Nur ‘Azah RA. Koestoer Ridho Irwansyah Santoso, Muhammad Agung Umar Abdul Aziz Wandono, Fajar Ari Yulianto Sulistyo Nugroho