Parametric CAD Modelling of Aircraft Wings for FEA Vibration Analysis

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ISSN Print: 2327-4352
ISSN Online: 2327-4379
www.scirp.org/journal/jamp
E-mail: jamp@scirp.org

"Parametric CAD Modelling of Aircraft Wings for FEA Vibration Analysis"
written by Shengyong Zhang, Mike Mikulich,
published by Journal of Applied Mathematics and Physics, Vol.9 No.5, 2021

has been cited by the following article(s):

[1]	Simulation of vibration based model using Finite Element Analysis (FEA) method
	AIP Conference Proceedings, 2023

[2]	Vibration Analysis Projects of Lumped-Parameter and Distributed-Parameter Systems
	2022 ASEE Annual Conference & Exposition, 2022

[3]	Design and characteristics study of an aircraft tapered wing
	International Journal of Mechanical Engineering, 2022

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