Zobrazeno 1 - 9
of 9
pro vyhledávání: '"Md. Nizam Dahalan"'
Publikováno v:
Journal of Advanced Research in Fluid Mechanics and Thermal Sciences. 89:142-153
Computational tools have led and helped researchers in providing advanced results, notably in rotorcraft research, as flow around the helicopter is dominated by complex aerodynamics and flow interaction phenomena. This research work aimed to evaluate
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::87384eff9729869e387266b9d4b6c792
https://doi.org/10.37934/arfmts.89.1.142153
https://doi.org/10.37934/arfmts.89.1.142153
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
Autor:
P. Segard, N. A. R. Nik Mohd, Shuhaimi Mansor, Shabudin Mat, Md. Nizam Dahalan, Mohd Nazri Mohd Nasir, Khushairi Amri Kasim
Publikováno v:
International Journal of Automotive and Mechanical Engineering; Vol 16 No 3 (2019): July-Sept; 6958-6970
Delta wing is a triangular-shaped platform that can be applied into the unmanned aerial vehicle (UAV) or drone applications. However, the flow above the delta wing is governed by complex leading-edge vortex structures which result in complicated aero
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::21cd49d4b7ff2da0b33d655cd78a5627
https://doi.org/10.15282/ijame.16.3.2019.10.0522
https://doi.org/10.15282/ijame.16.3.2019.10.0522
Publikováno v:
International Journal of Automotive and Mechanical Engineering. 17
Induction system or also known as the breathing system is a sub-component of the internal combustion system that supplies clean air for the combustion process. A good design of the induction system would be able to supply the air with adequate pressu
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c6d91fa90860a2c024df199b8236bd76
https://doi.org/10.15282/ijame.17.1.2020.10.0565
https://doi.org/10.15282/ijame.17.1.2020.10.0565
Publikováno v:
International Journal of Automotive and Mechanical Engineering. 15:5161-5177
Diffusing S-shaped ducts are critical components in modern vehicle, primarily employed in directing the airflow to the engine. It links the air box and the engine in a very restricted place. The air flow through an S-duct is complex in nature, which
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3fd52d82a4f849f3ee52f3826ce25b10
https://doi.org/10.15282/ijame.15.2.2018.2.0399
https://doi.org/10.15282/ijame.15.2.2018.2.0399
Autor:
Mazuriah Said, Md. Nizam Dahalan, Ainullotfi Abdul-Latif, Shuhaimi Mansor, Tholudin Mat Lazim, Shabudin Mat, Mohd Fahmi B. Abdullah
Publikováno v:
55th AIAA Aerospace Sciences Meeting.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5fa0c94276db7bd7597e25f0cd6601a1
https://doi.org/10.2514/6.2017-0326
https://doi.org/10.2514/6.2017-0326
Experimental Investigation on Blunt-Edged UTM Delta Wing VFE-2 Configurations at Low Reynolds Number
Autor:
Md. Nizam Dahalan, Shuhaimi Mansor, Mazuriah Said, Muhammad Zal Aminullah Daman Huri, Ainullotfi Abdul-Latif, Shabudin Mat
Publikováno v:
International Review of Mechanical Engineering (IREME). 12:255
The flow behaviour over the upper surface of a blunt-edged delta wing is mainly governed by a complicated leading edge vortex. This paper presents an experimental investigation on blunt-edged UTM VFE-2 delta wing model at low Reynolds numbers. The pr
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ec794681e5c6915261ad8f9d46856e4b
https://doi.org/10.15866/ireme.v12i3.13235
https://doi.org/10.15866/ireme.v12i3.13235
Autor:
Wan Khairuddin Wan Ali, Norazila Othman, Tholudin Mat Lazim, Wan Zaidi Wan Omar, Shuhaimi Mansor, Zurriati Mohd Ali, Ainullotfi Abdul-Latif, Mastura Abd Wahid, Mohd. Nazri Bin Nasir, Shabudin Mat, Muhammad Zaki Bin Abdul Manaf, Md. Nizam Dahalan
Publikováno v:
International Review of Mechanical Engineering (IREME). 12:263
This paper discusses the impact of the external store on the aerodynamic performance of the light aircraft model in the subsonic region. Light aircrafts are commonly used for pilots training, survey, leisure and transportation. To date, there have be
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3966ef972b7c9b81803b823279c7dc47
https://doi.org/10.15866/ireme.v12i3.13574
https://doi.org/10.15866/ireme.v12i3.13574
Publikováno v:
Jurnal Teknologi. 71
This paper presents the performance of a piezoelectric Synthetic Jet Actuator (SJA) in quiescent flow. Pulse jet velocity and vorticity were taken as the parameter to evaluate the performance of SJA. PIV measurements on the jet flow at the orifice ex
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::49ea2414a87bb5d79384e5e4e1fef851
https://doi.org/10.11113/jt.v71.3712
https://doi.org/10.11113/jt.v71.3712