Modelling of impact on sandwich structure for fast maintenance loops
In the aeronautical field, sandwich structures are widely used for secondary structures like flaps or landing gear doors. The modeling of low velocity/low energy impact, which can lead to a decrease of the structure strength by 50%, remains a designer’s main problem. Since this type of impact has th...
Main Authors: | Castanie, Bruno, Aminanda, Yulfian, Schwob, Cyrille |
---|---|
Format: | Conference or Workshop Item |
Language: | English |
Published: |
2012
|
Subjects: | |
Online Access: | http://irep.iium.edu.my/26648/ http://irep.iium.edu.my/26648/1/Article_ICAS2012.pdf |
Similar Items
-
Experimental study of the strength of sandwich structure with honeycomb core
by: Aminanda, Yulfian, et al.
Published: (2011) -
Design, construction, and testing of an open-loop low-speed wind tunnel
by: Muhammad Adnin, Mat Bahari
Published: (2012) -
Prediction of energy absorption capability of curved panel structure; for wing leading edge study
by: Omar, Norihan, et al.
Published: (2012) -
Spring-back of thick uni-directional carbon fibre reinforced composite laminate for aircraft structure application
by: Zakaria, Mohd Hafizu, et al.
Published: (2018) -
Modeling and structural analysis of three-dimensional wing
by: Mohd Zakuan, Muhammad Amir Mirza, et al.
Published: (2019)