Results 1 to 10 of about 388 (137)

Accuracy of Determining Stress Intensity Factors in Some Numerical Programs [PDF]

open access: yesActa Polytechnica, 2001
At present, there are many programs for numerical analysis of cracks, in particular for determining stress intensity factors. Analyses of a single-edge cracked beam and flat plate with a semielliptical surface crack are presented in this study to examine
M. Vorel, E. Leidich
doaj   +3 more sources

ANALYSIS AND APPLICATION OF THREE-DIMENSIONAL CRACK GROWTH BASED ON FRANC3D

open access: yesJixie qiangdu, 2018
The basic theory and solution flow of Franc3D were firstly focused,then elliptical embedded crack and semielliptical surface crack were employed to verify the stress intensive factor calculation accuracy from Franc3D and typical sheet problem was ...
AI ShuMin   +3 more
doaj   +1 more source

Potentials and limitations in finite element based crack propagation analysis using FRANC3D [PDF]

open access: closed, 2020
About 80% to 95% of all structural failures occur due to a fatigue mechanism1. Accurate fatigue assessment is therefore of great importance. This thesis focuses on a finite element analysis based approach, implemented in the program FRANC3D, to ...
Jonas Haeg, Filip Elfving
openalex   +2 more sources

Experimental and Numerical Research on 3D Crack Growth in Rocklike Material Subjected to Uniaxial Tension [PDF]

open access: yesJournal of Geotechnical and Geoenvironmental Engineering - ASCE, 2013
Uniaxial tension experiments on precracked rocklike samples and the related numerical simulations using FRANC3D were performed to investigate the growth mechanism of three-dimensional (3D) cracks in rocks under tension as well as the strength and failure
Yujing Jiang
exaly   +4 more sources

A Comparative Analysis of 3D Software for Modeling Fatigue Crack Growth: A Review

open access: yesApplied Sciences (Switzerland)
Fatigue crack growth modeling is critical for assessing structural integrity in various engineering applications. Researchers and engineers rely on 3D software tools to predict crack propagation accurately.
Abdulnaser Mohammed Alshoaibi   +1 more
exaly   +3 more sources

Three-dimensional Fatigue Crack Propagation Analysis of Aircraft Thin-walled Structures Under Out-of-plane Loading

open access: yesHangkong gongcheng jinzhan, 2022
Some thin-walled structures in aircraft structures inevitably bear out-of-plane bending,affecting the safety of aircraft significantly.The FRACN3D-ABAQUS simulation method is adopted to carry out such research work.Effects of boundary restraint and ...
ZENG Weipeng   +5 more
doaj   +1 more source

Three-Dimensional Surface Crack Growth of Maraging Steel Spherical Pressure Shell

open access: yesJournal of Marine Science and Engineering, 2021
This study focused on the three-dimensional surface crack growth of a spherical pressure shell. Eight maraging steel 18Ni (250) samples were fabricated and tested, and the fatigue crack growth rate curves were obtained.
Yongmei Zhu, Rujun Li, Jiahao Yang
doaj   +1 more source

Comparison of fatigue crack growth of riveted and bonded aircraft lap joints made of Aluminium alloy 2024-T3 substrates – A numerical study [PDF]

open access: yes, 2017
Aircraft lap joints play an important role in minimizing the operational cost of airlines. Hence, airlines pay more attention to these technologies to improve efficiency.
Crespo Artiaga, Daniel   +2 more
core   +1 more source

Stress intensity factors and crack propagation path under mixed mode conditions [PDF]

open access: yesJournal of Structural and Construction Engineering, 2016
Use of crack propagation principles based on SIFs (stress intensity factors) is among the most common methods of fracture mechanic engineering. SIF is an important parameter in fracture analysis. In analyzing elastic fracture, SIF reveals the stress near
Ramin Faridvand, Mohammad Taghi Kazemi
doaj   +1 more source

Surrogate Modeling of High-Fidelity Fracture Simulations for Real-Time Residual Strength Predictions [PDF]

open access: yes, 2011
A surrogate model methodology is described for predicting, during flight, the residual strength of aircraft structures that sustain discrete-source damage.
Hochhalter, Jacob D.   +4 more
core   +3 more sources

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