Articles
Thermal Performance of Analysis of Serpentine Channel Cold Plate for 18650 Cylindrical Lithium-Ion Battery
Fitri Wahyuni;
James Julian;
Rainer Samuel Fourlando;
Riki Hendra Purba;
Fathin Muhammad Mahdhudhu;
Elvi Armadani;
Nely Toding Bunga
Jurnal Asiimetrik: Jurnal Ilmiah Rekayasa Dan Inovasi Volume 8 Number 1 (2026)
Publisher : Fakultas Teknik Universitas Pancasila
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DOI: 10.35814/asiimetrik.v8i1.9430
This research evaluates the thermal performance of a liquid cooling system with serpentine channel inlets for an 18650 cylindrical lithium-ion battery module. The study analyzed an eight-cell module with a baseline configuration and variations featuring two, three, and four serpentine curves using computational fluid dynamics simulations validated against previous experiments. A fixed mass flow rate of 0.0001 kg/s was applied. Results showed all configurations-maintained battery temperatures below 37.5°C, preventing thermal runaway. The Baseline configuration achieved the lowest maximum temperature of 37.447°C and the highest performance factor (J/F factor) of 0.053. The two serpentine curves offered the best temperature uniformity (1.114°C) and highest heat transfer coefficient. Although more serpentine curves reduced maximum temperature, they increased pressure drop, decreasing the J/F factor. The study concludes that the serpentine cold plate design effectively manages thermal containment, with the two-curve configuration providing the best balance of heat transfer and temperature stability.
Analisis Motor Listrik Tipe Synchronous dengan Metode Komputasi
James Julian;
Fitri Wahyuni;
Lomo Mula Tua;
Nely Toding Bunga
Jurnal Asiimetrik: Jurnal Ilmiah Rekayasa Dan Inovasi Volume 3 Nomor 1 Tahun 2021
Publisher : Fakultas Teknik Universitas Pancasila
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DOI: 10.35814/asiimetrik.v3i1.1879
In the current technological development, the electric motor is the most popular in various industrial applications. Electric motors today have evolved very quickly and have a significant impact on the lives of the wider community. The use of environmentally friendly and efficient energy is one of the reasons why this motorbike has become a pioneer of technological advances, especially in the automotive world. This research focuses on conducting a comprehensive analytical study on one type of electric motor, namely synchronous because it is widely applied in various conditions today. The analysis was carried out using a computational method by applying the finite element as a method of solving the magnetic field case involving Maxwell's equations and its impact on the torque generated in this synchronous motor. From the computation results, it is found that this synchronous motor does have a high torque when the magnetic field flux works constantly at 0.015 Wb. With an average torque generated by this synchronous motor of 1.5 kW.
Karakteristik Kekerasan Lasan Titik Gesekan dan Pengadukan pada Paduan Aluminium 5052-H112
Armansyah;
Juri Saedon;
Ferdyanto;
Nely Toding Bunga;
James Julian
Jurnal Asiimetrik: Jurnal Ilmiah Rekayasa Dan Inovasi Volume 4 Nomor 2 Tahun 2022
Publisher : Fakultas Teknik Universitas Pancasila
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DOI: 10.35814/asiimetrik.v4i1.3183
Issues in friction stir spot welding focus mainly on the mechanical characteristic affected by its Hardness. This Hardness must be maintained by evenly temperature distribution in weld zones during welding. The process parameters are mainly responsible for the development of the hardness of the friction stir spot weld. This study presented the hardness evaluations on the friction stir spot weld via the Hardness-Vickers test and analysis of the temperature distribution in the weld zones via the finite element method. The workpiece samples used in this study were Aluminium alloy 5052-H112 with a thickness of 2 millimeters in the lap-shear mode based on 3 main parameters at low and high levels of parameters configuration. The results obtained via the Hardness-Vickers tests exhibited a value of 42-HV located in the middle of the spot-weld center using a low-level parameters configuration. This value increased to 64-HV around the vicinity of the keyhole. And then the value decreased to 53-HV outside the keyhole, about 6 millimeters from the spot-weld center. Using high-level parameter configuration, the Hardness-Vickers value increased to 61-HV in the middle of the spot-weld center. The value then increased to 76-HV in the vicinity of the keyhole. Furthermore, the value decreased at 60-HV outside the keyhole, which ca 6 millimeters away from the spot-weld center. The temperature distribution of the weld zones achieved 480 oC in the vicinity of the keyhole using the low-level parameter configuration. Slowly, the temperature declined to 380 oC at 6 mm away from the friction spot-weld center in the HAZ. Using the high-level parameters configuration, the temperature distribution reached 540 oC in SZ, and slowly reduced to 425 oC in HAZ. Based on the results, it was found that by using high-level parameters configuration the hardness of the friction stirs spot weld exhibited better Hardness-Vickers value and evenly temperature distribution in the weld zones.
Characterization of the Co-Flow Jet Effect as One of the Flow Control Devices
James Julian;
Waridho Iskandar;
Fitri Wahyuni;
Ferdyanto;
Nely Toding Bunga
Jurnal Asiimetrik: Jurnal Ilmiah Rekayasa Dan Inovasi Volume 4 Nomor 2 Tahun 2022
Publisher : Fakultas Teknik Universitas Pancasila
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DOI: 10.35814/asiimetrik.v4i1.3437
The computational study discusses the application of the co-flow jet technique as a fluid flow control device on the NACA 0015 airfoil. The numerical equation used is the RANS equation with the k-ε turbulence model. There are three variations of the mesh proposed in this paper. The first variation is a fine mesh with 100,000 elements. The second variation is a medium mesh with 50,000 elements. Meanwhile, the third variation is coarse mesh with 25,000 elements. Based on the mesh independence test results, the mesh with the lowest error value is the fine mesh. Co-flow jet is proven to control fluid flow on the upper side of NACA 0015. Co-flow jet can also improve the aerodynamic performance of NACA 0015 by increasing Cl and decreasing Cd. The increase in Cl was 114% and the decrease in Cd was 24%. The fluid flow separation on the upper side of the airfoil can also be handled well by the co-flow jet.
Aerodynamic Performance Improvement on NACA 4415 Airfoil by Using Cavity: Peningkatan Performa Aerodinamika NACA 4415 dengan Menggunakan Cavity
James Julian;
Waridho Iskandar;
Fitri Wahyuni;
Nely Toding Bunga
Jurnal Asiimetrik: Jurnal Ilmiah Rekayasa Dan Inovasi Volume 5 Nomor 1 Tahun 2023
Publisher : Fakultas Teknik Universitas Pancasila
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DOI: 10.35814/asiimetrik.v5i1.4259
This study uses a numerical method to analyze the cavity's use on the airfoil's trailing edge and the aerodynamic effects it generates. The type of airfoil used is NACA 4415. The variations in the Reynolds number examined in this study are 2×105 and 3×105. The governing equation is the Reynolds Averaged Navier-Stokes paired with the k-ε turbulence model. This study concludes that the cavity can increase Cl in the airfoil but cannot delay the stall. The increase in Cd is also a negative effect of using a cavity in the airfoil. The cavity can increase Cl by increasing the pressure on the lower side near the trailing edge. Meanwhile, the cavity increases Cd because it creates a separation of the fluid flow, forming a vortex when viewed in a streamlined form of fluid flow.
The The Effect of Micro Geometry with Various Forms as Passive Flow Control in NACA 4415: Pengaruh Geometri Berukuran Mikro Dengan Variasi Bentuk Sebagai Kontrol Aliran Pasif di NACA 4415
James Julian;
Rizki Aldi Anggara;
Fitri Wahyuni;
Nely Toding Bunga
Jurnal Asiimetrik: Jurnal Ilmiah Rekayasa Dan Inovasi Volume 5 Nomor 2 Tahun 2023
Publisher : Fakultas Teknik Universitas Pancasila
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DOI: 10.35814/asiimetrik.v5i2.4678
This study investigates the effect of variations in the micro geometry with various forms as passive flow control devices on the aerodynamic capability of the airfoil. Micro-cylinder, micro-slat, and micro-cube are installed close to the leading edge of the NACA 4415 airfoil as a micro geometric variation of passive flow control devices with a predetermined diameter of 3% c located at coordinates x= 0% c and y= 8 %c of the leading edge of the airfoil. The Reynolds number used in this study is Re = with AoA variations from 0°-30°. This study's results show a decrease in Cl of 12% with a micro-cylinder, 26% with a micro-slat, and 28% with a micro-cube. In addition, the Cd produced by using the variation of the device micro geometry has increased significantly. Thus, the final result is a lift-to-drag ratio of more petite than the without micro. In the streamlined contour shown when the airfoil is at a high angle of attack, the use of micro geometric variations of passive flow control devices can have an effect that causes reduced recirculation that occurs in the airfoil. However, the impact of these devices is not optimal, resulting in a reduction in the aerodynamic capability of the NACA 4415 airfoil.
Analysis of the Use of Bio Flap on NACA 4415 with Numerical Methods: Analisis Penggunaan Bio Flap pada NACA 4415 dengan Metode Numerik
James Julian;
Saphira Anggraita Siswanto;
Fitri Wahyuni;
Nely Toding Bunga
Jurnal Asiimetrik: Jurnal Ilmiah Rekayasa Dan Inovasi Volume 5 Nomor 2 Tahun 2023
Publisher : Fakultas Teknik Universitas Pancasila
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DOI: 10.35814/asiimetrik.v5i2.4768
This study was conducted using the Computational Fluid Dynamics (CFD) method using the Reynolds Averaged Navier Stokes (RANS) approach. The type of airfoil used in this study is the asymmetry NACA 4415 airfoil type. In this paper, computational tests were carried out on the airfoil with the addition of bionic flaps on its trailing edge. This study's update tests three variations of the Reynolds number: Re = 106, Re = 5 × 105, and Re = 3 × 105. The airfoil test was carried out at AoA 0°–25°. The addition of bionic flaps causes a decrease in lift performance at low AoA, but at high AoA, it can increase lift performance on airfoils. In addition, adding a bionic flap on the airfoil can delay the occurrence of a stall. At AoA 10°–13°, the Cd of the three variations of the Reynolds number experiences an increase in performance. Then, from this computational test, the resulting Coefficient moment (Cm) is a pitch down because the torque is below zero.
NUMERICAL STUDY ON THERMAL PERFORMANCE OF MINI-CHANNEL COOLING ON CYLINDRICAL LITHIUM-ION BATTERY COOLING SYSTEM
Elvi Ermadani;
James Julian;
Bima Rakha Adhitama;
Fitri Wahyuni;
Riki Hendra Purba;
Fathin Muhammad Mahdhudhu;
Adi Winarta
Logic : Jurnal Rancang Bangun dan Teknologi Vol. 26 No. 1 (2026): March
Publisher : Unit Publikasi Ilmiah, P3M, Politeknik Negeri Bali
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DOI: 10.31940/logic.v26i1.86-94
This study investigates how a liquid-based cooling configuration influences the thermal behavior of a cylindrical lithium-ion (Li-ion) battery pack through numerical analysis. The work underscores the crucial role of proper thermal regulation to maintain operational safety and prolong battery lifespan in high-demand applications such as electric vehicles (EVs). Three cooling-channel diameters—4, 6, and 8 mm—were examined under a 5C discharge condition. The findings indicate that the 8 mm channel offers the most advantageous performance, delivering the lowest maximum temperature, quicker thermal stabilization, and improved temperature uniformity. Conversely, the 4 mm channel resulted in elevated peak temperatures and a temperature gradient (ΔT) of 8.3 °C, which may intensify hotspot formation and accelerate cell degradation. Overall, the results emphasize the importance of selecting an appropriate cooling-channel diameter to effectively mitigate thermal stress.
Implementasi Pompa Sentrifugal DC dalam Upaya Penghematan Energy Listrik Guna Mendukung Proses Budidaya pada Komunitas Ikan Meruyung Fish Farm
James Julian;
Sekar Yuliana;
Fitri Wahyuni;
Rifqi Ramadhani;
Rizki Anggara;
Raysa Nisa
Journal of Community Development Vol. 6 No. 1 (2025): August
Publisher : Indonesian Journal Publisher
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DOI: 10.47134/comdev.v6i1.1428
Pompa air membantu menjaga kualitas air dengan memastikan oksigen tersedia dalam jumlah yang cukup, mengeliminasi sisa makanan dan kotoran, serta menyebarkan muatan organik secara merata pada kolam. Program pengabdian masyarakat yang diajukan bertujuan untuk menyediakan pompa sentrifugal DC yang inovatif dan ramah lingkungan guna mendukung keberlanjutan budidaya ikan air tawar. Meruyung fish farm adalah salah satu pelaku usaha yang memiliki permasalahan yang signifikan mengenai keterbatasan energi dalam kegiatan operasional budidaya ikan. Tim penelitian menawarkan solusi dengan melakukan pemasangan atau pengimplementasian Pompa Sentrifugal DC hemat energi. Pada program ini, kegiatan dilakukan melalui tiga tahap, yaitu tim peneliti melakukan survey lapangan untuk pengukuran, kemudian melaksanakan proses desain dan perancangan sistem, dan terakhir pengimplementasian pemasangan dan sosialisasi. Ketika tahap pelaksanaan kegiatan, sistem Pompa Sentrifugal DC berjalan dengan baik. Alat uji coba menunjukkan konsumsi daya 82 watt dengan debit 50 LPM. Hal tersebut menunjukkan bahwa alat telah bekerja dan sudah sesuai dengan harapan dari mitra.
Pembuatan Pelet Ikan Mandiri Dalam Upaya Menyejahterakan Kelompok Pembudidaya Ikan Konsumsi Air Tawar Sawangan-Parung
James Julian;
Rena Sari;
Fitri Wahyuni;
Anton Prabowo;
Regina Lumbantoruan;
Putty Hapidzha
Journal of Community Development Vol. 6 No. 1 (2025): August
Publisher : Indonesian Journal Publisher
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DOI: 10.47134/comdev.v6i1.1429
Kegiatan pengabdian masyarakat ini bertujuan untuk membantu kelompok pembudidaya ikan konsumsi air tawar di Sawangan-Parung dalam memproduksi pakan ikan secara mandiri guna mengurangi biaya operasional. Biaya pakan ikan diketahui mencapai 70-80% dari total biaya produksi, sehingga pengurangan biaya ini menjadi penting untuk keberlanjutan usaha mereka. Solusi yang diberikan adalah pembuatan mesin pelet dengan kapasitas produksi 20 kg per jam, yang memanfaatkan bahan baku lokal seperti tepung ikan, dedak, tepung jagung, serta bahan tambahan lainnya. Pelaksanaan kegiatan ini terdiri dari tiga tahap. Tahap pertama adalah survei lapangan untuk memahami kondisi dan kebutuhan pembudidaya. Tahap kedua melibatkan perancangan dan pembuatan mesin pelet yang mudah digunakan oleh pembudidaya setempat, serta efisien dalam memanfaatkan bahan baku lokal. Tahap terakhir berupa sosialisasi dan pendampingan kepada pembudidaya dalam menggunakan mesin tersebut.Hasil dari kegiatan ini menunjukkan keberhasilan mesin pelet dalam menurunkan biaya produksi pakan, dari Rp13.000 menjadi Rp8.000 per kilogram. Penurunan ini secara signifikan membantu mengurangi biaya operasional pembudidaya, sehingga meningkatkan efisiensi dan profitabilitas usaha budidaya ikan air tawar mereka.