An isogeometric finite element approach for thermal bending and buckling analyses of laminated composite plates

2017 ◽  
Vol 179 ◽  
pp. 35-49 ◽  
Author(s):  
Loc V. Tran ◽  
M. Abdel Wahab ◽  
Seung-Eock Kim
Keyword(s):  
Finite Element ◽  
Laminated Composite ◽  
Composite Plates ◽  
Laminated Composite Plates ◽  
Finite Element Approach ◽  
Thermal Bending ◽  
Element Approach

Design and Analysis of an Aircraft Composite Hinge Bracket Using Finite Element Approach

2014 ◽  
Vol 629 ◽  
pp. 158-163
Author(s):  
Wai Chee Mun ◽  
Ahmad Rivai ◽  
Omar Bapokutty
Keyword(s):  
Finite Element ◽  
Composite Structures ◽  
Laminated Composite ◽  
Composite Plates ◽  
Metallic Structures ◽  
Aircraft Structures ◽  
Finite Element Approach ◽  
Heterogeneous Nature ◽  
Element Approach ◽  
Margin Of Safety

The use of composite materials in aircraft structures have been increasing for the past decade. The anisotropic and heterogeneous nature of composites remains a major challenge to the design and analysis of composite aircraft structures. Composite structures require a different design approach compared to the design of metallic structures. This paper aims to provide a step by step definitive guide to design and analyze composite structures using finite element approach. A simplified design model for the composite structural design was used to analyze an aircraft composite hinge bracket. The composite hinge bracket which is made of IM7/8552 laminated composite plates was successfully designed with a margin of safety of 0.216 and a weight savings of 43.77 percent was estimated.

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