Zobrazeno 1 - 10
of 18
pro vyhledávání: '"M. A. Moelyadi"'
Publikováno v:
IOP Conference Series: Earth and Environmental Science. 1108:012001
The airfoil profile of this study is based on plant morphology, which is rarely modeled in airfoil profiling. Designing, modeling, and analyzing the aerodynamics of one of the projected morphological parts of the banana leaf midrib that forms a 45-de
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5d5d750b4c192ea9f09fa6cfca1bf488
https://doi.org/10.1088/1755-1315/1108/1/012001
https://doi.org/10.1088/1755-1315/1108/1/012001
Autor:
M A Moelyadi, M F Afthon
Publikováno v:
AVIA. 2
According to the objectivity of UAV helicopter, endurance is a valuable performance. To increase the endurance, we need to decrease the helicopter required power. Within the research scope in vertical movement only, 5 parameters of blades planform de
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5bb80e11861df0dcaa93719caaebb5f2
https://doi.org/10.47355/avia.v2i1.12
https://doi.org/10.47355/avia.v2i1.12
Publikováno v:
THE 8TH INTERNATIONAL SEMINAR ON AEROSPACE SCIENCE AND TECHNOLOGY – ISAST 2020.
In this paper, avionics subsystems as well as its integrations for High Altitude Long Endurance (HALE) UAV ITB V4 is presented. There are several factors that must be considered in designing & selecting electronics for HALE UAV such as environment, m
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0d0a2dd0090ba91282e6adfef1d6df99
https://doi.org/10.1063/5.0059968
https://doi.org/10.1063/5.0059968
Publikováno v:
IOP Conference Series: Materials Science and Engineering. 1173:012049
This paper deals with the preliminary design of bionic flapping wing vehicle. The design is driven by its requirement and objective namely the maximum weight should be less than 0.5 kg with 1.5 m wingspan. In the conceptual design, the wing planform,
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::efbb995857b922eeb34927d3b64a9c93
https://doi.org/10.1088/1757-899x/1173/1/012049
https://doi.org/10.1088/1757-899x/1173/1/012049
Publikováno v:
IOP Conference Series: Materials Science and Engineering. 1173:012055
One of the factors for the long endurance of high altitude long endurance (HALE) of an unmanned aerial vehicle (UAV) that belong to Institut Teknologi Bandung, Indonesia or called as HALE UAV ITB is the design of battery and solar panel. This paper d
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c1b568eb5af47b39f102029a6768df20
https://doi.org/10.1088/1757-899x/1173/1/012055
https://doi.org/10.1088/1757-899x/1173/1/012055
Publikováno v:
AIP Conference Proceedings.
This paper aims to design a small-scale, compact supersonic wind tunnel nozzle using the method of characteristics and perform computational fluid dynamics (CFD) simulations to validate the design. The wind tunnel is designed to have a test section o
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f07484045190ba1f1d24c74860d8b002
https://doi.org/10.1063/5.0003727
https://doi.org/10.1063/5.0003727
Publikováno v:
IOP Conference Series: Materials Science and Engineering. 645:012021
In the past few years, the usage of Unmanned Aerial Vehicles (UAVs) aircraft has increased significantly, but the need for UAVs with higher performance is increasing also. Therefore, all systems of the UAVs must be developed to have high efficiency,
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::fd8cbe8cc1dd1fdec9cd1507ed16eabd
https://doi.org/10.1088/1757-899x/645/1/012021
https://doi.org/10.1088/1757-899x/645/1/012021
Publikováno v:
Journal of Engineering and Technological Sciences, Vol 45, Iss 1, Pp 47-60 (2013)
Journal of Engineering and Technological Sciences, Vol 45, Iss 1 (2013)
Journal of Engineering and Technological Sciences, Vol 45, Iss 1 (2013)
The unsteady flow behavior and time-dependent aerodynamic characteristics of the flapping motion of a bird’s wing were investigated using a computational method. During flapping, aerodynamic interactions between bird wing surfaces and surrounding f
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::f6574f8afeed8a7777011673d2a9affa
http://journals.itb.ac.id/index.php/jets/article/view/619/340
http://journals.itb.ac.id/index.php/jets/article/view/619/340
Autor:
M. Agoes Moelyadi, E. Irsyad Lukman
Publikováno v:
Journal of Physics: Conference Series. 1005:012050
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7adc5ff377ebcb5b1532dd393effc9a4
https://doi.org/10.1088/1742-6596/1005/1/012050
https://doi.org/10.1088/1742-6596/1005/1/012050
Publikováno v:
Journal of Physics: Conference Series. 1005:012015
Tube Launched UAV with expandable tandem-wing configuration becomes one of the most interesting topic to be investigated. Folding wing mechanism is used due to the requirements that the UAV should be folded into tubular launcher. This paper focuses o
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5a0dd638016d5e62245d3a540c014aa6
https://doi.org/10.1088/1742-6596/1005/1/012015
https://doi.org/10.1088/1742-6596/1005/1/012015