F
Faizal Mustapha
Researcher at Universiti Putra Malaysia
Publications - 193
Citations - 3037
Faizal Mustapha is an academic researcher from Universiti Putra Malaysia. The author has contributed to research in topics: Finite element method & Composite number. The author has an hindex of 25, co-authored 177 publications receiving 2305 citations. Previous affiliations of Faizal Mustapha include University of Sheffield & National Defense University.
Papers
More filters
Journal ArticleDOI
Mechanical Performance and Corrosion Behaviour of Diffusion-Bonded A5083 Aluminium and A36 Mild Steel with Gallium Interlayer
Asmawi Ismail,Nurul Husna Othman,Mazli Mustapha,Mohamed Shuaib Mohamed Saheed,Zaki Abdullah,Musa Muhammed,Asmalina Mohamed Saat,Faizal Mustapha +7 more
TL;DR: In this article , the authors investigated the mechanical performance and corrosion behaviour of a diffusion-bonded A5083 aluminium/A36 mild steel dissimilar joint with a Gallium (Ga) interlayer.
Journal ArticleDOI
Damage Detection Using Prior Wavelet Decompositions
TL;DR: In this paper, the effectiveness of wavelet decomposition of Lamb wave responses for structural damage detection was investigated. But the work was conducted as part of the European Union project ARTIMA.
In this study, the behaviour of laminated composite plates, fiber Kevlar
TL;DR: In this paper, the effect of the deflection and stresses on the plate thickness-to-length ratio, aspect ratio, modulus ratio, fiber orientation and the number of layers were observed.
Journal ArticleDOI
Structural fault diagnosis of UAV based on convolutional neural network and data processing technology
TL;DR: In this article , the root mean square error (RMSE) feature was used to select the Y-axis acceleration data, which exhibits significant changes across different damage cases, and a convolutional neural network is used to identify the damage based on the vibration data.
Journal ArticleDOI
Parametric Study on Cohesive Element for Composite Fuselage Model
TL;DR: In this paper, a numerical simulation on a new fabrication miniature composite fuselage structure-a woven composite laminated with an adhesively bonded butt joint under the axial compression loading is presented.