Calculation of hybrid joints used in modern aerospace structures
The state – of - the art of aeronautical structures show that parts are manufactured and subsequently assembled with the use of fasteners and/ or bonding. Adhesive bonding is a key technology to low weight, high fatigue resistance, robustness and an attractive design for cost structures.The paper re...
Main Authors: | Marcel STERE, Daniela BARAN |
---|---|
Format: | Article |
Language: | English |
Published: |
National Institute for Aerospace Research “Elie Carafoli” - INCAS
2011-12-01
|
Series: | INCAS Bulletin |
Subjects: | |
Online Access: | http://bulletin.incas.ro/files/stere_baran_v3_iss_4_full.pdf |
Similar Items
-
Experimental and Numerical Investigation of Effect of Static and Fatigue Loading on Behavior of Different Double Strap Adhesive Joint Configurations in Fiber Metal Laminates
by: Muhammad Azeem, et al.
Published: (2022-03-01) -
Theoretical Analysis of Stress Distribution in Bonded Single Strap and Stiffened Joints
by: Behnam Ghoddous -
A Review of Structural Adhesive Joints in Hybrid Joining Processes
by: Sofia Maggiore, et al.
Published: (2021-11-01) -
The Hybrid Joints between an FRP Panel and a Steel Panel through Tubular Reinforcements: A Methodology for Interlaminar Stress Calculations
by: Franklin Domínguez, et al.
Published: (2020-06-01) -
Mechanical properties of hybrid joints in timber structures
by: Kosuke Imakawa, et al.
Published: (2022-06-01)