MODELING STRATEGY OF SANDWICH STRUCTURE WITH HETEROGENEOUS CORE UNDER IMPACT LOADING
Sandwich composite structure (relatively a thick core inserted between two thin laminated composite faceplates) have been used to fabricate important components in aircraft structure, e.g. aileron, nacelle, etc. As these components are prone to either low or high-velocity impact due to tooling and e...
Saved in:
Main Author: | Pratama, Valdo |
---|---|
Format: | Theses |
Language: | Indonesia |
Online Access: | https://digilib.itb.ac.id/gdl/view/68996 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Institution: | Institut Teknologi Bandung |
Language: | Indonesia |
Similar Items
-
FAILURE MODES OF CYLINDRICAL CORRUGATED CORE SANDWICH UNDER QUASI-STATIC AXIAL COMPRESSIVE AND INTERNAL PRESSURE LOADINGS
by: Sultan Bakhtari, Jorghy -
Impact modeling of foam cored sandwich plates with ductile or brittle faceplates
by: Sridhar, Idapalapati, et al.
Published: (2013) -
Structural response of metal foam cored sandwich structures
by: Tay, Yong Zhen.
Published: (2012) -
THE RESPONSE OF CYLINDRICAL SANDWICH STRUCTURES INSPIRED BY BAMBOO UNDER UNIAXIAL COMPRESSIVE LOAD
by: Jihad Ummul Quro, M -
NUMERICAL STUDY OF T-JOINT DAMAGE IN SANDWICH COMPOSITE STRUCTURE UNDER QUASI-STATIC LOADING
by: Fitriyah, Lailatul