Effects of Unbalanced Lamination Parameters on the Static Aeroelasticity of a High Aspect Ratio Wing
In this paper, in order to understand the influence of the unbalanced coefficient of composite laminates on the static aeroelasticity of high aspect wings, a series of numerical simulation calculations were carried out, and this work wants to provide some reference for the structural design of aircr...
Saved in:
Main Authors: | JinYang Li, JunLi Wang, ZhiGui Ren, WeiFeng Wei |
---|---|
Format: | Article |
Language: | English |
Published: |
Wiley
2021-01-01
|
Series: | International Journal of Aerospace Engineering |
Online Access: | http://dx.doi.org/10.1155/2021/3949078 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
Effect of Aeroelastic Tailoring Design on Wing Mode
by: Yajuan He, et al.
Published: (2023-01-01) -
Failure Analysis and Optimization Design of Wing Skin Unbalanced Lay-Up
by: Junli Wang, et al.
Published: (2022-01-01) -
Thermal Aeroelastic Tailoring for Laminated Panel with Lamination Parameters and JAYA Algorithm
by: Peng Jin, et al.
Published: (2022-01-01) -
Geometrical Nonlinear Aeroelastic Stability Analysis of a Composite High-Aspect-Ratio Wing
by: Chang Chuan Xie, et al.
Published: (2008-01-01) -
Static Aeroelastic Characteristics of Morphing Trailing-Edge Wing Using Geometrically Exact Vortex Lattice Method
by: Sen Mao, et al.
Published: (2019-01-01)