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Original Article
Conceptual design and simulation validation based finite element optimisation for tubercle leading edge composite wing of an unmanned aerial vehicle
Ernnie Illyani Basria, Faizal Mustaphaa, Mohamed Thariq Hameed Sultana,b,c,
Corresponding author
thariq@upm.edu.my

Corresponding authors.
, Adi Azriff Basria, Mohd Firdaus Abasa, Mohd Shukry Abdul Majidd, Kamarul Arifin Ahmada,e,
Corresponding author
aekamarul@upm.edu.my

Corresponding authors.
a Department of Aerospace Engineering, Faculty of Engineering, Universiti Putra Malaysia, 43400 UPM Serdang, Selangor Darul Ehsan, Malaysia
b Laboratory of Biocomposite Technology (BIOCOMPOSITE), Institute of Tropical Forestry and Forest Products (INTROP), Universiti Putra Malaysia, 43400 UPM Serdang, Selangor Darul Ehsan, Malaysia
c Aerospace Malaysia Innovation Centre (944751-A), Prime Minister's Department, MIGHT Partnership Hub, Jalan Impact, 63000 Cyberjaya, Selangor, Malaysia
d School of Mechatronic Engineering, Universiti Malaysia Perlis, Pauh Putra Campus, 02600 Arau, Perlis, Malaysia
e Aerospace Manufacturing Research Centre (AMRC), Universiti Putra Malaysia, 43400 UPM Serdang, Selangor, Malaysia
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ISSN: 22387854
Original language: English
The statistics are updated each day
Year/Month Html Pdf Epub Total
2019 November 0 0 0 0
2019 October 0 0 0 0
2019 September 1 2 0 3
2019 August 20 22 6 48
Journal of Materials Research and Technology

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