Zobrazeno 1 - 10
of 21
pro vyhledávání: '"Firman Hartono"'
Autor:
Iman K. Reksowardojo, Long H. Duong, Rais Zain, Firman Hartono, Septhian Marno, Wawan Rustyawan, Nelliza Putri, Wisasurya Jatiwiramurti, Bayu Prabowo
Publikováno v:
Energies, Vol 13, Iss 24, p 6570 (2020)
Biofuels as alternative fuels in today’s world are becoming increasingly important for the reduction of greenhouse gases. Here, we present and evaluate the potential of a new alternative fuel based on the conversion of medium-chain fatty acids to b
Externí odkaz:
https://doaj.org/article/c6e82ec396d74fc3880f7989656ec17f
Publikováno v:
Journal of Advanced Research in Fluid Mechanics and Thermal Sciences. 85:14-23
This study aims to design an axial turbine rotor blade and predict the turbine performance at preliminary design stage. Quasi three dimensional method was applied to design including blade to blade flow analysis. The blade profile uses a NACA 0015 ai
Autor:
Long H. Duong, Nelliza Putri, Rais Zain, Septhian Marno, Firman Hartono, Wawan Rustyawan, Bayu Prabowo, Iman K. Reksowardojo, Wisasurya Jatiwiramurti
Publikováno v:
Energies
Volume 13
Issue 24
Energies, Vol 13, Iss 6570, p 6570 (2020)
Volume 13
Issue 24
Energies, Vol 13, Iss 6570, p 6570 (2020)
Biofuels as alternative fuels in today&rsquo
s world are becoming increasingly important for the reduction of greenhouse gases. Here, we present and evaluate the potential of a new alternative fuel based on the conversion of medium-chain fatty a
s world are becoming increasingly important for the reduction of greenhouse gases. Here, we present and evaluate the potential of a new alternative fuel based on the conversion of medium-chain fatty a
Autor:
Dana Herdiana, Firman Hartono
Publikováno v:
Jurnal Teknologi Dirgantara. 18
Telah dilakukan pengujian perdana dari pesawat LSU-05 buatan LAPAN dimana hasil evaluasi pengujian terdapat kekurangan yaitu pada saat pesawat melakukan manuver, hal tersebut diakibatkan oleh beberapa faktor. Salah satu faktor adalah kurangnya koefis
Publikováno v:
AVIA. 2
This paper explains about aerodynamic design of a single stage gas generator turbine for a small turbojet engine. The design requirement is that the turbine must be able to deliver power output of 150 kW at 0.814 kg/s gas mass flow, with turbine inle
Publikováno v:
THERMOFLUID X: 10th International Conference on Thermofluids 2019.
To design a radial compressor there are many geometry parameters that must be considered. Leading edge shape, trailing edge shape and of course the shape of the unit blade itself. Geometry parameters of the impeller defined by its operation condition
Publikováno v:
AIP Conference Proceedings.
Following the accomplishment of Thrust Benchmarking System (TBS) as a low-cost and easy-to-manufacture instrument for UAV electric propulsion performance measurement, further development is made by adding some new features which includes mechanical s
Publikováno v:
International Journal of Fluid Machinery and Systems. 10:447-456
Publikováno v:
International Journal of Fluid Machinery and Systems. 9:362-369
Publikováno v:
AIP Conference Proceedings.
The present study is aimed to determine the effect of pitch chord ratio on an axial turbine rotor blade design. The selected swirling flow criterion used in this study is mixed vortex. There are two models of turbine rotor that used in this study and