UAV NACA4415 Wing Structural Performance Analysis Subjected to External Aerodynamic Load Using Schrenk’s Approximation
semanticscholar(2019)
摘要
1 Department of Aerospace Engineering, Faculty of Engineering, Universiti Putra Malaysia, 43400 UPM Serdang, Selangor Darul Ehsan, Malaysia 2 Laboratory of Biocomposite Technology, Institute of Tropical Forestry and Forest Products (INTROP), Universiti Putra Malaysia, 43400 UPM Serdang, Selangor Darul Ehsan, Malaysia 3 Aerospace Malaysia Research Centre (AMRC), Universiti Putra Malaysia, 43400 UPM Serdang, Selangor Darul Ehsan, Malaysia 4 Aerospace Malaysia Innovation Centre (944751-A), A Prime Minister’s Department, MIGHT Partnership Hub, Jalan Impact 63000 Cyberjaya, Selangor, Malaysia
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