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Shuhaimi Mansor

Researcher at Universiti Teknologi Malaysia

Publications -  94
Citations -  424

Shuhaimi Mansor is an academic researcher from Universiti Teknologi Malaysia. The author has contributed to research in topics: Wind tunnel & Aerodynamics. The author has an hindex of 9, co-authored 91 publications receiving 354 citations. Previous affiliations of Shuhaimi Mansor include Loughborough University.

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The role of education and training in absorptive capacity of international technology transfer in the aerospace sector

TL;DR: In this paper, the role of education and training in the aerospace sector for establishing sufficient levels of absorptive capacity in newly industrialized countries is substantial and forms a fundamental part of a nation's ability to establish and cultivate absorptive capacities on a national or organization-specific level.
Posted ContentDOI

COVID-19 epidemic in Malaysia: Impact of lock-down on infection dynamics

TL;DR: Three different epidemic forecasting models was used to generate forecasts of COVID-19 cases in Malaysia using daily reported cumulative case data up until 1st April 2020 from the Malaysia Ministry of Health, suggesting the epidemic may peak between middle of April to end of May 2020.
Book

Estimation of Bluff Body Transient Aerodynamic Loads: Using an Oscillating Model Rig

TL;DR: In this paper, a method for the estimation of transient aerodynamic derivatives from dynamic wind tunnel tests using time response data is presented, where the aerodynamic derivative is considered to act as a stiffness and damping to the model motion.
Journal ArticleDOI

Experimental study of yaw angle effect on the aerodynamic characteristics of a road vehicle fitted with a rear spoiler

TL;DR: In this article, the yaw angle effect on the aerodynamic performance of a hatchback model fitted with a roof spoiler was investigated, and the results of the surface pressures indicate that the changes in the flow around the rear slanted body are the main factors affecting the aerodynamics performance of the model using the spoiler.
Journal Article

Application of intelligent controller in feedback control loop for aircraft pitch control

TL;DR: The investigation into the development of hybrid control scheme for pitch control of aircraft system shows that, the PID-type fuzzy logic controller perform the best performance compared to classical controller technique, Proportional-Integral-Derivative (PID).