The effect of delamination in free vibration responses of adhesively bonded spar wingskin joints-Reference-Cited by-同舟云学术

The effect of delamination in free vibration responses of adhesively bonded spar wingskin joints

Published:2020-12-15 Issue: Volume: Page:1-18
ISSN:1539-7734
Container-title:Mechanics Based Design of Structures and Machines
language:en
Short-container-title:Mechanics Based Design of Structures and Machines

Author:

Mishra P. K.¹,Pradhan A. K.²,Pandit M. K.²,Panda S. K.¹

Affiliation:

1. Department of Mechanical Engineering, Centre for Advanced Post Graduate Studies, BPUT, Odisha, India

2. School of Mechanical Sciences, IIT, Bhubaneswar, Odisha, India

Publisher

Informa UK Limited

Subject

Mechanical Engineering,Mechanics of Materials,Ocean Engineering,Condensed Matter Physics,Aerospace Engineering,Automotive Engineering,General Mathematics,Civil and Structural Engineering

Link

https://www.tandfonline.com/doi/pdf/10.1080/15397734.2020.1858869

Reference37 articles.

1. Vibration Damping of Adhesively Bonded Joints

2. Reduced Basis Eigenvalue Solutions for Damaged Structures∗

3. Progressive Failure Analysis Using Global-Local Coupling Including Intralaminar Failure and Debonding

4. A robust optimization for damage detection using multiobjective genetic algorithm, neural network and fuzzy decision making

5. Modal parameter identification and vibration based damage detection of a multiple cracked cantilever beam

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