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All Journal Journal of Engineering and Technological Sciences Mesin Jurnal Teknologi Dirgantara Jurnal Nasional Teknik Elektro dan Teknologi Informasi SCIENTIFIC JOURNAL OF NURSING RESARCH Indonesian Journal of Aerospace Warta Ardhia: Jurnal Transportasi
Hari Muhammad
Aerospace Engineering Study Program, Institut Teknologi Bandung, Jalan Ganesha No. 10 Bandung, Jawa Barat 40132, Indonesia
Aerospace Engineering Astronomy Chemical Engineering, Chemistry & Bioengineering Computer Science & IT Control & Systems Engineering Electrical & Electronics Engineering Energy Engineering Mechanical Engineering Medicine & Pharmacology Nursing Physics Public Health Transportation Veterinary

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Journal : mesin

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PREDIKSI DAN ANALISIS KESTABILAN GERAK LONGITUDINAL KAPAL BERSAYAP WING-IN-SURFACE EFFECT Muhammad, Hari
Mesin Vol 19, No 1 (2004)
Publisher : Mesin

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Abstract

This paper discusses the stability of Wing-in-Surface-Effect (WiSE) craft. The aerodynamic parameters of new WiSE craft jointly designed by the Agency for the Assessment and Application of Technology, Indonesian Aerospace Ltd. and Institute of Technology Bandung are estimated using software Digital Datcom of the US Air Force. The aerodynamic parameters are used to predict the longitudinal stability characteristics of the WiSE craft. The surface effect on some aerodynamic parametes that influence the longitudinal stability of the WiSE craft will be discussed in this paper.
RANCANG BANGUN MICRO AIR VEHICLE KONFIGURASI TAILLESS Mulyanto, Taufiq; Wijaya, Arinta H; Muhammad, Hari
Mesin Vol 23, No 2 (2008)
Publisher : Mesin

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Abstract

Nowadays, Micro Air Vehicle (MAV) is mostly developed for surveillance purpose, either for military or civilian. In this article, a design and building of a MAV will be presented. A tailless configuration was chosen. The design and build process started with a study of several design parameters of existing MAVs. Then, it is followed by initial sizing, detail design and production of the MAV. In general, the designed MAV could meet the design requirements and objectives stated. Some preliminary tests had shown that the basic flying characteristics was sufficiently good, although further development still has to be done. The design and build process was also able to evaluate the implementation of some aircraft design formula and method being implemented to design MAV.
PREDIKSI DAN ANALISIS KESTABILAN GERAK LONGITUDINAL KAPAL BERSAYAP WING-IN-SURFACE EFFECT Hari Muhammad
Mesin Vol. 19 No. 1 (2004)
Publisher : Mesin

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

Abstract

This paper discusses the stability of Wing-in-Surface-Effect (WiSE) craft. The aerodynamic parameters of new WiSE craft jointly designed by the Agency for the Assessment and Application of Technology, Indonesian Aerospace Ltd. and Institute of Technology Bandung are estimated using software Digital Datcom of the US Air Force. The aerodynamic parameters are used to predict the longitudinal stability characteristics of the WiSE craft. The surface effect on some aerodynamic parametes that influence the longitudinal stability of the WiSE craft will be discussed in this paper.
RANCANG BANGUN MICRO AIR VEHICLE KONFIGURASI TAILLESS Taufiq Mulyanto; Arinta H Wijaya; Hari Muhammad
Mesin Vol. 23 No. 2 (2008)
Publisher : Mesin

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

Abstract

Nowadays, Micro Air Vehicle (MAV) is mostly developed for surveillance purpose, either for military or civilian. In this article, a design and building of a MAV will be presented. A tailless configuration was chosen. The design and build process started with a study of several design parameters of existing MAVs. Then, it is followed by initial sizing, detail design and production of the MAV. In general, the designed MAV could meet the design requirements and objectives stated. Some preliminary tests had shown that the basic flying characteristics was sufficiently good, although further development still has to be done. The design and build process was also able to evaluate the implementation of some aircraft design formula and method being implemented to design MAV.
Co-Authors Akhmad Farid Widodo Alex J. Sepnov Alex J. Sepnov Arifianto, Ony Arinta H Wijaya Aziz Fathurrahman Bambang Riyanto Trilaksono Duong V. Dung Duong V. Dung Faturrohim, Luqman Hilman Samputra Javensius Sembiring Javensius Sembiring, Javensius Jenie, Yazdi I Lavi Rizki Zuhal Leonardo Gunawan Leonardo Gunawan, Leonardo Luqman Faturrohim Mahardi Sadono Mohamad Hasan Bashory Mulyanto, Taufiq Novi Andria Novi Andria, Novi Poetro, Ridanto Eko Ridanto Eko Poetro Ridanto Eko Poetro Robertus Heru Triharjanto Robertus Heru Triharjanto Rully Medianto Samputra, Hilman Toto Indriyanto Triharjanto, Robertus Heru Widodo, Akhmad Farid Widowati, Widowati Wijaya, Arinta H Yazdi I. Jenie Yazdi Ibrahim Jenie Zuhai, Lavi Rizki Zuhal, Lavi R.