- Aerodynamics and Fluid Dynamics Research
- Wind and Air Flow Studies
- Aerospace and Aviation Technology
- Fluid Dynamics and Turbulent Flows
- Computational Fluid Dynamics and Aerodynamics
- Vehicle Dynamics and Control Systems
- Fluid Dynamics and Vibration Analysis
- Aerodynamics and Acoustics in Jet Flows
- Aerospace Engineering and Control Systems
- Vehicle Noise and Vibration Control
- Air Traffic Management and Optimization
- Guidance and Control Systems
- Plasma and Flow Control in Aerodynamics
- Vehicle emissions and performance
- Mechanical Engineering and Vibrations Research
- Aeroelasticity and Vibration Control
- Advanced Aircraft Design and Technologies
- Biomimetic flight and propulsion mechanisms
- Aerospace Engineering and Energy Systems
- Composite Structure Analysis and Optimization
- Evacuation and Crowd Dynamics
- Building Energy and Comfort Optimization
- Real-time simulation and control systems
- Concrete and Cement Materials Research
- Geotechnical and construction materials studies
University of Technology Malaysia
2014-2023
Hospital Pulau Pinang
2023
Universiti Teknologi MARA
2021-2023
University of Technology
2015-2017
Vaughn College of Aeronautics and Technology
2011-2016
Malaysia University of Science and Technology
2015
Loughborough University
2006-2010
Selangor Business School
2004
Abstract COVID-19 epidemic in Malaysia started as a small wave of 22 cases January 2020 through imported cases. It was followed by bigger mainly from local transmissions resulting 651 The following saw unexpectedly three digit number daily mass gathering urged the government to choose more stringent measure. A limited lock-down approach called Movement Control Order (MCO) immediately initiated whole country way suppress trajectory. causes major socio-economic disruption thus ability forecast...
International technology transfer of advanced and knowledge their subsequent absorption is crucial to firms in developing nations. This research paper aims further enhance the understanding operationalization absorptive capacity construct. In rigorous review existing literature, organizational routines were found play a significant role enhancing an organization's capacity. We present our conceptualization necessitated as dynamic capability Necessitated Absorptive Capacity model. contributes...
The role of education and training in the aerospace sector for establishing sufficient levels absorptive capacity newly industrialized countries is substantial forms a fundamental part nation's ability to establish cultivate on national or organization-specific level. Successful international technology transfer as well absorption knowledge into recipient organizations, depends prodigiously types policy adopted all groups individuals specifically outlined this paper. conducted literature...
Purpose The purpose of this study is to investigate the flow on blunt-edged delta wing Vortex Flow Experiment (VFE-2) configuration in wind tunnel testing. characteristics exhibits differently from sharp-edges where primary vortex developed at certain chord-wise position apex. Design/methodology/approach A model VFE-2 has been replicated with main chord length 1.3 meters two sets leading-edge radius. experiments were performed Universiti Teknologi Malaysia sized 2 × 1.5 m test section...
Resin waste, which is the residual material from integrated circuit (IC) packages investigates widespread usage in electronics industry. Hence, identifying efficient alternative methods to recycle this resin waste will significantly bolster endeavor for a sustainable environment construction applications. This study presents utilization of foamed concrete-based (FC-RW) non-loading walls. The process involved grinding (RW) obtained STMicroelectronics Sdn. Bhd. into particles sized 0.5 ± 0.02...
The performance of a wing-in-ground effect craft depends mostly on its wing configuration. aerodynamic characteristics compound wings were numerically investigated during the ground effect. was divided into three parts with one rectangular in middle and two reverse taper anhedral angle at sides. NACA 6409 airfoil employed as section wings. Three-dimensional computational fluid dynamics applied scheme. k-turbulent model used for turbulent ?ow over surface. results aspect ratio 1, attack 2...
Finite element method is increasingly used in the analysis of aircraft structures, including Unmanned Aerial Vehicles (UAVs). The structural model for finite however needs to be validated order ensure that it correctly represents physical behaviour actual structure. In this work, a case study straight, unswept and untapered wing structure made composite material subjected aerodynamic loading was modelled analysed using method. Four-noded, reduced integration shell elements were used, with...
Vehicle drivability is defined as the smoothness of a vehicle's operation at will driver under all driving conditions.Currently, evaluation conducted through subjective ratings-based test standard which derived from established procedures.Human rating can be inconsistent due to physical health conditions and individual preferences.This study determine possibility using longitudinal acceleration arrange an objective assessment.Vehicle vehicle ratings four expert evaluators.A was evaluated...
In automotive industry, thin walled beam is widely used to build vehicles structure. Vehicle structure built by joining beams using various welding techniques. The usage of in important improve vehicle performance offering better strength-to-weight ratio. However the application will cause few drawbacks When or loaded with compression load, at certain limit it undergo local global buckling. Another problem when joined other beams, show unexpected deformation which called joint flexibility....
Rear-roof spoiler is commonly used for improving the aerodynamic performance of road vehicles. This study aims to investigate effect strip-type rear-roof on hatchback The main parameter was inclination angle spoiler. A computational fluid dynamics (CFD) method used. numerically obtained results were compared experimental data validation CFD method. effectively reduced lift at positive by causing surface pressure near roof-spoiler junction increase. However, its unfavourable when configured...
A method for the estimation of transient aerodynamic data from dynamic wind tunnel tests has been developed and employed in study unsteady response simple automotive type bodies.The paper describes facility analysis techniques reports results a parametric model rear slant angle influence C-pillar strakes.The is shown to exhibit damped, self-sustained self-excited behaviour.The are compared with quasi-steady predictions based on conventional balance through calculation derivative...
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 aerodynamics research development in Universiti Teknologi Malaysia, low speed (UTM-LST). Steady load balance flow visualization tests conducted at Reynolds numbers 0.5, 1, 1.5 × 10 6 , respectively. measurement number was also 5 m/s. During experiments, laser with smoke visualizations...
The COVID-19 pandemic has had dramatic effects on the socio-economic and well beings of Malaysians. objective study is to find university students both technical side, such as sufficiency infrastructure internet support online teaching learning (T&L), social stress level focus study. nationwide effect Malaysian varsities was conducted at end 2020. There are many important issues uncovered in this ranging from internet-ready programs, psychological perspectives. It shall provide...
The effect of rear-roof spoiler on the aerodynamic drag performance simple hatchback model has been investigated for a range pitch angles. RANS based CFD method was utilized. Validation done by comparing results Ahmed without to experimental data. beneficial influence at positive inclination angle below 5°. Above that angle, increases with angle. mechanism how influences identified through extensive flow visualization.
Thin walled structure is widely used in designing light weight vehicle. For automotive industry, an important characteristic to increase performance of a Vehicle structures are built from thin beams by joining them using various methods and techniques. structure, its stiffness greatly depends on joint stiffness. However, beam difficult predict accurately due buckling effect. Once the joined form it will expose flexibility A lot researches had been done behaviors analytically numerically....
This paper will describe the aerodynamic characteristic of complete aircraft equipped with conventional tail and V-tail configurations. Based on lateral-directional stability, introduction dihedral angle can significantly affect yaw stability derivative an aircraft. The wind tunnel test was conducted for sideslip angle, from -25◦ to 25◦ results were used verify CFD works. Good agreements achieved at a lower which is below 15◦. Then, be study flow field around region figure out effect...
This paper discusses further the effects of Reynolds number, angle attack and leading edge bluntness on flow topology above delta wing VFE-2 configurations. In this project two models differentiated by its radius to mean aerodynamics chord ratio 0.15 0.3, namely medium large wing, were tested in Universiti Teknologi Malaysia wind tunnel. The relationship between primary vortex occurrence a secondary called inner round-edged wings are discussed. bluntness, number both systems discussed paper....