Product
Help
Pricing
About
Jobs
Log in
Get started
Author
Add to collection
Bing Yan
Institution:
Chinese Aeronautical Establishment
Observed institutions:
Universidade do Porto,
Chinese Aeronautical Establishment,
Nanjing University of Aeronautics and Astronautics
ORCID:
0000-0002-7608-0209
Observed ORCID:
0000-0002-7608-0209
OpenAlex ID:
A5007983307
Buckling and post-buckling analysis of composite stiffened panels: A ten-year review (2014–2023)
2024
·
Guijia Zhang
, Yuanyuan Hu
, et al.
·
Thin-Walled Structures
·
46
Experiment and mesoscopic modelling on the dynamic compressive behaviors of a new carbon fiber-reinforced cement-based composite
2022
·
Zhangyu Wu
, Jinhua Zhang
, et al.
·
Cement and Concrete Composites
·
46
A design methodology of composite scarf repairs using artificial intelligence
2023
·
Bing Yan
, Mingbo Tong
, et al.
·
Composites Part B Engineering
·
18
Experimental study on the mechanical properties of laminates made of thin carbon fiber plies
2020
·
Bing Yan
, Shuhua Zhu
, et al.
·
Composite Structures
·
18
An Improved Semi-analytical Method for the strength prediction of composite bonded scarf repairs
2022
·
Bing Yan
, Mingbo Tong
, et al.
·
Composite Structures
·
16
Compression‐After‐Impact Performance of CFRP Laminates With Pre‐Embedded Delamination Subjected to Low‐Velocity Impact and Bolted Reinforcement
2025
·
Guijia Zhang
, Mingbo Tong
, et al.
·
Polymer Composites
·
4
PDF
A methodology to predict the strength of composite scarf joints based on ductile adhesives
2026
·
Bing Yan
, Song Pan
, et al.
·
Composite Structures
Show more works
View as search
Works count:
7
Citation count:
148
H-index:
5
I10-index:
5
Year
Topic
Type
