Simple and Fast Method to Calculate Shape Factors of Stiffened Panels Repaired with Composites-Reference-Cited by-同舟云学术

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Simple and Fast Method to Calculate Shape Factors of Stiffened Panels Repaired with Composites

Published:2019-05 Issue:3 Volume:32 Page:04019007
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Hosseini-Toudeshky Hossein¹,Seyedzadeh Seyed Sobhan²,Ghayour Mohammadhossein²

Affiliation:

1. Professor, Dept. of Aerospace Engineering, Amirkabir Univ. of Technology, 424 Hafez Ave., Tehran 15875-4413, Iran (corresponding author).

2. Master Student, Dept. of Aerospace Engineering, Amirkabir Univ. of Technology, 424 Hafez Ave., Tehran 15875-4413, Iran.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0000981

Reference21 articles.

1. Computation of the stress intensity factors for repaired cracks with bonded composite patch in mode I and mixed mode

2. Bonded Repair of Aircraft Structures

3. Fatigue Crack Growth in Stiffened Panels under Pressure Loading

4. Boundary element analysis of stiffened panels with repair patches

5. Finite element fatigue propagation of induced cracks by stiffeners in repaired panels with composite patches

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Effect of constraints on stress intensity factor for dissimilar metal plate with centre crack under uniform tension;Materials Today Communications;2020-03

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