Zobrazeno 1 - 10
of 35
pro vyhledávání: '"Shabudin Mat"'
Publikováno v:
Energies, Vol 15, Iss 19, p 6925 (2022)
For the past decade, research on vertical axis wind turbines (VAWTs) has garnered immense interest due to their omnidirectional characteristic, especially the lift-type VAWT. The H-rotor Darrieus VAWT operates based on the lift generated by aerofoil
Externí odkaz:
https://doaj.org/article/2436adca22684014a3d06fa51c348096
Autor:
Shabudin Mat, I. S. Ishak, Tholudin Mat Lazim, Shuhaimi Mansor, Mazuriah Said, Abdul Basid Abdul Rahman, Ahmad Shukeri Mohd. Kamaludim, Romain Brossay
Publikováno v:
Advances in Mechanical Engineering, Vol 6 (2014)
This paper presents wind tunnel experiment on two delta wing configurations which are differentiated by their leading edge profiles: sharp and round-edged wings. The experiments were performed as a part of the delta wing aerodynamics research develop
Externí odkaz:
https://doaj.org/article/6dde64860b874ce59fa3721dd63631d6
Publikováno v:
Acta Polytechnica, Vol 44, Iss 2 (2004)
The main objective of the present work is to study the effect of an external store to a subsonic fighter aircraft. Generally most modern fighter aircraft is designed with an external store installation. In this project a subsonic fighter aircraft mod
Externí odkaz:
https://doaj.org/article/4a41745652e14ca4ad0326bce09cbe26
Publikováno v:
Acta Polytechnica, Vol 43, Iss 5 (2003)
The main objective of the present work is to study the effect of an external store on a subsonic fighter aircraft. Generally most modern fighter aircrafts are designed with an external store installation. In this study, a subsonic fighter aircraft mo
Externí odkaz:
https://doaj.org/article/2366aceb5b3f4ea98b180057e63fd2de
Publikováno v:
Aircraft Engineering and Aerospace Technology. 95:1081-1091
Purpose The flow topology for multi-disciplinary configuration (MULDICON) wing is very complicated and nonlinear at low to high angle of attack (AOA). This paper aims to provide the correlation between the unsteadiness and uncertainties of the flow t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::599304da21d3e81d25f34545f560145d
https://doi.org/10.1108/aeat-03-2022-0092
https://doi.org/10.1108/aeat-03-2022-0092
Autor:
null Rafiqi Daniel Ramadhan Mariaprakasam, null Shabudin Mat, null Pakharuddin Mohd Samin, null Norazila Othman, null Mastura Ab Wahid, null Mazuriah Said
Publikováno v:
Journal of Advanced Research in Fluid Mechanics and Thermal Sciences. 101:11-36
Reducing aerodynamic drag in automobiles has been one of the focuses in automotive industry as it will increase vehicles performance and reduce power consumption which subsequently save the environment. Drag is a force that tend to pull the vehicle b
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9a700d914e826efc37c3ec6f8bd31a46
https://doi.org/10.37934/arfmts.101.1.1136
https://doi.org/10.37934/arfmts.101.1.1136
Autor:
Mohammed Munif Hasan, Shabudin Mat
Publikováno v:
International Journal for Research in Applied Science and Engineering Technology. 10:952-959
The effective use of wind-tunnel testing in determining aerodynamic properties of a body is very much dependent upon the reliability and speed with which wind-tunnel data can be reduced. The operating efficiency of the wind tunnels is substantially i
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::be69ee01bc4cd45db83fee96a6856b0c
https://doi.org/10.22214/ijraset.2022.47097
https://doi.org/10.22214/ijraset.2022.47097
Autor:
null Leong Chee Hang, null Nur Athirah Nadwa Rosli, null Mastura Ab Wahid, null Norazila Othman, null Shabudin Mat, null Mohd Zarhamdy Md Zain
Publikováno v:
Journal of Advanced Research in Fluid Mechanics and Thermal Sciences. 96:82-95
The purpose of this study is to see the feasibility of using Computational Fluid Dynamic (CFD) analysis over wind tunnel testing for propeller performance measurement. Computational Fluid Dynamic (CFD) analysis is conducted on APC 6X4E propeller and
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4ffe62abf30b3598802f7861d4942b60
https://doi.org/10.37934/arfmts.96.1.8295
https://doi.org/10.37934/arfmts.96.1.8295
Publikováno v:
Aircraft Engineering and Aerospace Technology. 93:127-138
Purpose This study aims to investigate the effects of propeller locations on the aerodynamic characteristics of a generic 55° swept angle sharp-edged delta wing unmanned aerial vehicle (UAV) model. Design/methodology/approach A generic delta-winged
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::35890175963a15a4f2b086cc82f8c510
https://doi.org/10.1108/aeat-11-2018-0279
https://doi.org/10.1108/aeat-11-2018-0279
Autor:
Shuhaimi Mansor, Shabudin Mat, N. A. R. Nik Mohd, M. Imai, Mazuriah Said, Mohd Nazri Mohd Nasir, Md. Nizam Dahalan
Publikováno v:
International Journal of Automotive and Mechanical Engineering. 17:8214-8223
This paper reports on flow visualisation and surface pressure measurements over the upper surface of a blunt-edged delta wing model at high angles of attack. The flow structure above the upper surface of the blunt-edged delta wing was found to be dif
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5334cd3462678e90482615eb02b5907c
https://doi.org/10.15282/ijame.17.3.2020.15.0619
https://doi.org/10.15282/ijame.17.3.2020.15.0619