Prediction of Residual Strength and Curvilinear Crack Growth in Aircraft Fuselages-Reference-Cited by-同舟云学术

Prediction of Residual Strength and Curvilinear Crack Growth in Aircraft Fuselages

Published:2002-08 Issue:8 Volume:40 Page:1644-1652
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Chen Chuin-Shan¹,Wawrzynek Paul A.²,Ingraffea Anthony R.²

Affiliation:

1. National Taiwan University, Taipei 10617, Taiwan, Republic of China

2. Cornell University, Ithaca, New York 14853

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/2.1836

Reference33 articles.

1. 2Chen, C.S. “Crack Growth Simulationand Residual StrengthPrediction in Thin Shell Structures,” Ph.D. Dissertation, School of Civil and Environmental Engineering,Cornell Univ., Ithaca,NY, Jan. 1999.

2. 3Potyondy, D. O. “A Methodology for Simulation of Curvilinear Crack Growth in Pressurized Shells,” Ph.D. Dissertation, School of Civil and Environmental Engineering,Cornell Univ., Ithaca,NY, Aug. 1993.

Cited by 12 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. Fatigue Behavior and Mechanism Study on Lugs of TC18 Titanium Alloy;Crystals;2023-08-29

2. Advanced crack tip field characterization using conjugate work integrals;International Journal of Fatigue;2023-04

3. Prediction of a Crack Growth Trajectory with Allowance for the Angular Distribution of the Small Components of the Tangential Stresses at a Crack Tip;Russian Metallurgy (Metally);2019-10

4. Fatigue crack deflection in cruciform specimens subjected to biaxial loading conditions;International Journal of Fatigue;2018-08

5. A review of T-stress and its effects in fracture mechanics;Engineering Fracture Mechanics;2015-01