Article Per Year (5 Year)
p-Index From 2020 - 2025
3.512
P-Index
This Author published in this journals
All Journal Bulletin of Electrical Engineering and Informatics Jurnal Aplikasi Bisnis dan Manajemen (JABM) E-Journal Jurnal RESTI (Rekayasa Sistem dan Teknologi Informasi) SINERGI: Jurnal Ilmiah Ilmu Manajemen Jurnal Pertahanan : Media Informasi tentang Kajian dan Strategi Pertahanan yang Mengedepankan Identity, Nasionalism dan Integrity JURNAL EDUCATION AND DEVELOPMENT NUSANTARA : Jurnal Ilmu Pengetahuan Sosial Jurnal Riset Informatika Jurnal Teknologi Dirgantara INSIST (International Series on Interdisciplinary Research) Journal of Robotics and Control (JRC) ASEAN Journal of Community Engagement Budapest International Research and Critics Institute-Journal (BIRCI-Journal): Humanities and Social Sciences Journal of Strategic and Global Studies Jurnal Multidisiplin Madani (MUDIMA) Journal Research of Social Science, Economics, and Management Indonesian Journal of Community Services Indonesian Journal of Aerospace
Bura, Romie O.
Universitas Pertahanan Republik Indonesia
Religion Aerospace Engineering Agriculture, Biological Sciences & Forestry Arts Humanities Astronomy Chemical Engineering, Chemistry & Bioengineering Civil Engineering, Building, Construction & Architecture Computer Science & IT Control & Systems Engineering Decision Sciences, Operations Research & Management Economics, Econometrics & Finance Education Electrical & Electronics Engineering Engineering Environmental Science Industrial & Manufacturing Engineering Languange, Linguistic, Communication & Media Law, Crime, Criminology & Criminal Justice Library & Information Science Mechanical Engineering Medicine & Pharmacology Physics Public Health Social Sciences Other

Published : 30 Documents Claim Missing Document
Claim Missing Document
Check
Articles

Found 5 Documents
Search
Journal : Indonesian Journal of Aerospace

 1 
Aerodynamic Characteristic Optimization on The Design of Anti - Ship Missile for Indonesian Fast - Attack Boat Dwiastuty, Fuji; Bura, Romie Oktovianus; Triharjanto, Robertus Heru
Indonesian Journal of Aerospace Vol. 17 No. 2 Desember (2019): Jurnal Teknologi Dirgantara
Publisher : BRIN Publishing

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.30536/j.jtd.2019.v17.a3157

Abstract

Missile is one of Indonesia 7 self – reliant main weapon system programs. Therefore research on the anti – surface ship missile system concept had been carried out at the Faculty of Defense Technology, Defense University. This research aims to abtain optimal design of anti – ship missile concept from previous research, i.e. 2 stages cruise missile with diameter of 0.36 m, total length of 5.19 m, cruise flight altitude of 17 m, and cruise flight speed of 0.88 Mach. The optimation is done on the missile’s aerodynamics characteristics to maximize its lift to drag ratio, which is one of the factor that determine the missile’s performance. Variables of nose cone shapes, number of wings, and body cross sections were chosen for evaluation of lift to drag ratio. The research found that nose cone shape did not affect the aerodynamic characteristics since the flight speed is subsonic. From the rest of the variables, it is found that the best configuration is missile with 2 wings with root length of 1.18 m, height of 0.79 m, and tip length of 0.71 m, elliptical body cross section, and the missile is to be flown at 6o angle of attack.
Numerical Investigation of Supersonic and Hypersonic Shock-Wave/Boundary-Layer Interactions Bura, Romie Oktovianus; Graham T. Roberts; Yufeng Yao; Neil D. Sandham
Indonesian Journal of Aerospace Vol. 23 No. 1 (2025): Indonesian Journal Of Aerospace
Publisher : BRIN Publishing

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.55981/ijoa.2025.12201

Abstract

Numerical simulations of 2-D supersonic and hypersonic laminar Shock-Wave/Boundary-Layer Interactions (SBLIs) were carried out by solving the Navier-Stokes (NS)equations using a compressible flow code over a wide range of Mach numbers and shockstrengths. The results obtained at Mach 2.0 and 7.73 were compared with experimentaldata. In addition, the numerical data were further analyzed using correlation laws derivedby previous researchers based on the free interaction concept, extended here to higherMach numbers. The results indicate that this concept is valid for separated laminar hypersonicflows with SBLIs. For interference heating, the correlation technique based on thewell-established power law relationship between peak heating and peak pressures yieldedencouraging results consistent with other correlations for laminar interference heating athypersonic speeds.
PERANCANGAN DAN ANALISIS INTEGRASI HYPERSONIC WAVERIDER–INLET SCRAMJET (DESIGN AND ANALYSIS OF HYPERSONIC WAVERIDER– SCRAMJET INLET INTEGRATION) Malik, Deden Ridwan; Bura, Romie Oktovianus
Indonesian Journal of Aerospace Vol. 12 No. 1 Juni (2014): Jurnal Teknologi Dirgantara
Publisher : BRIN Publishing

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

Abstract

Nowadays, several hypersonic vehicle designs have existed and waverider is one of them. Waverider has been introduced for more than 50 years yet only a few have been operated. This is due to several difficulties in design processes dan propulsion system integration. The present research was conducted by designing general wedgederived waverider and integrating it with scramjet inlet. The waverider design process is based on one-dimensional flowfield analysis, while the scramjet inlet integration is based on exergy analysis. Through this investigation, a design variable – Exergy Destruction Rate (EDR) - would be obtained to correlate the waverider design with the integration of scramjet inlet
CHARACTERIZATION OF SIZE AND SHAPE OF AMMONIUM PERCHLORATE PARTICLE FROM CHINA, SOUTH KOREA, AND INDONESIA AND THEIR INFLUENCES ON PROPERTIES OF PROPELLANT Hutauruk, Jones; Bura, Romie Oktovianus; Wibowo, Heri Budi
Indonesian Journal of Aerospace Vol. 18 No. 1 Juni (2020): Jurnal Teknologi Dirgantara
Publisher : BRIN Publishing

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.30536/j.jtd.2020.v18.a3346

Abstract

The aim of this study is to obtain characteristics of ammonium perchlorate particle that used in Rocket Technology Center (LAPAN). Characterization begin from the determination of particle size distribution with Particle Size Analyzer. The SEM is used to obtain information about the morphology of AP, furthermore, the results are reprocessed using ImageJ software to analyze the shape of AP particle, and the Surface area was obtained by using BET. Characteristic of AP such as particle size, shape, and surface area are important parameters because those are directly related to propellant combustion energy. Ammonium perchlorate was procured from China, South Korea, and Indonesia with a particle size of 200µm From this study, the particle size of APC200, APH200 and API200 was obtained, which are 265 µm, 236 µm, and 242 µm, with particle shape aggregate value of 0,68, 0,38 and 0,33, roundness of 0,57, 0,79,0,63, and surface area of 1,104 m2/g, 5,561 m2/g, and 2,972 m2/g.
DESAIN DAN PENGUJIAN INTAKE KONIKAL SISTEM PROPULSI RAMJET PADA KECEPATAN SUPERSONIK (DESIGN AND TEST OF CONICAL INTAKE OF RAMJET PROPULSION SYSTEM AT SUPERSONIC SPEED) Sofyan, Sofyan; Bura, Romie Oktovianus
Indonesian Journal of Aerospace Vol. 13 No. 1 Juni (2015): Jurnal Teknologi Dirgantara
Publisher : BRIN Publishing

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

Abstract

Riset ini bertujuan untuk mendesain intake supersonik untuk aplikasi sistem propulsi ramjet. Desain intake ramjet sangat penting bagi proses pembakaran dalam ruang bakar mesin ramjet. Dalam desain intake konikal ini, kondisi Mach 2 dijadikan sebagai acuan, dengan kompresi eksternal. Penelitian ini juga menguji intake ramjet dalam terowongan angin supersonik. Desain dilakukan dengan menempatkan gelombang kejut pada bibir cowl intake untuk memperoleh pressure recovery yang tinggi dan gaya hambat serendah mungkin. Hasil desain analitik dibandingkan dengan hasil numerik pada berbagai kondisi intake – subkritikal, kritikal, dan superkritikal. Hasil numerik juga divalidasi dengan eksperimen model. Intake yang didesain memberi pressure recovery sebesar 0,93, namun hasil ini cukup berbeda dengan hasil eksperimental. Ini disebabkan karena efisiensi kompresi tidak diikutkan dalam proses desain.
Co-Authors - Sofyan A. Octavian Agus Bayu Utama Amarulla Octavian Amperiawan, Gita Andi Fathurrachman Batara Sulo Andiarti, Rika Arif Nur Hakim Artono, Endro Aziz Ikhsan Bachtiar Boshra Algandouz Dadang Gunawan Deden Ridwan Malik Dwiastuty, Fuji Dwicahyono, Taufik Eko Priamadi Eko Putro, Idris Emhamed Boras Faisa Lailiyul Mutho' Affifah Faishal Irfan Farraz, Muhammad Gamantyo Hendrantoro Graham T. Roberts Hakim, Arif Nur Hanif, Azizul Haryanto A.R, Timbul Henry Setyanto Heri Budi Wibowo Heri Yansyah Herma Yudhi Irwanto Hutauruk, Jones Irdam Ahmad Irvan Arianto Randa Lembang Irwanto, Herma Yudhi Jamal Elbakay Elbakay Larasmoyo Nugroho Lilis Mariani, Lilis Luhut Simbolon Luky Adrianto Lutfi Adin Affandi Malik, Deden Ridwan Marimin , Martharaharja, Januar Arief Maspin Apit Mirad Fahri Muhammad Adnan Utomo Muhammad Farraz Muhammad Hanifudin Al Fadli Neil D. Sandham Octavian, A. Oka Sudiana Pujo Widodo, Pujo R Djoko Andreas Navalino Raden Andhika Ajiesastra Ratno Nuryadi Riska Nurtantyo Sarbini Salwa Muftah Eljamay Sarjito, Aris Shahed Muftah Shahrazad Eteer Siswo Hadi Sumantri Sofyan Sofyan Sovian Aritonang Sudiana, Oka Timbul Haryanto AR Triharjanto, Robertus Heru Utama, Yudki Utomo, Muhammad Adnan Wisnu Ari Adi Yudki Utama Yufeng Yao Yusgiantoro, Purnomo Zainal Abidin Sahabuddin, Zainal Abidin