Show/Hide Menu
Hide/Show Apps
Logout
Türkçe
Türkçe
Search
Search
Login
Login
OpenMETU
OpenMETU
About
About
Open Science Policy
Open Science Policy
Open Access Guideline
Open Access Guideline
Postgraduate Thesis Guideline
Postgraduate Thesis Guideline
Communities & Collections
Communities & Collections
Help
Help
Frequently Asked Questions
Frequently Asked Questions
Guides
Guides
Thesis submission
Thesis submission
MS without thesis term project submission
MS without thesis term project submission
Publication submission with DOI
Publication submission with DOI
Publication submission
Publication submission
Supporting Information
Supporting Information
General Information
General Information
Copyright, Embargo and License
Copyright, Embargo and License
Contact us
Contact us
The influence of cyclic fatigue damage on the fracture toughness of carbon-carbon composites
Date
1996-01-01
Author
Ozturk, A
Metadata
Show full item record
This work is licensed under a
Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License
.
Item Usage Stats
173
views
0
downloads
Cite This
The influence of cyclic loads on the fracture toughness of a tightly woven carbon-carbon composite was investigated as a function of stress levels. Results of fracture toughness tests were correlated with microstructural examination using scanning electron microscopy (SEM). Values for the stress intensity factor, K-Ic, were determined using the ASTM single-edge notched bend test. Results were discussed in terms of the effects of applied cyclic stress levels and the relationship of the load-displacement curves. The fracture toughness of the composite remained unaffected when the maximum tensile load in the fatigue cycle was up to 80% of the static tensile strength. However, a decrease in the fracture toughness was determined when it was exposed to cyclic loads above this threshold stress level. Changes in texture associated with cyclic fatigue were determined in the matrix of this composite. Copyright (C) 1996 Elsevier Science Limited
Subject Keywords
Carbon-carbon
,
Microstructure
,
Fracture toughness
,
Fatigue
URI
https://hdl.handle.net/11511/64150
Journal
COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING
DOI
https://doi.org/10.1016/1359-835x(96)00035-8
Collections
Department of Metallurgical and Materials Engineering, Article
Suggestions
OpenMETU
Core
The effect of double austenitization on the microstructure and toughness of AISI M2 high speed steel
Ögel, Bilgehan (1998-06-01)
In this study, the effect of double austenitization on microstructure and toughness of AISI M2 high speed steel was investigated. For double austenitization treatment, the specimens, which are hardened initially at 1220 degrees C and quenched in air, were hardened for a second time in the temperature range 1150 - 1050 degrees C. For comparison purposes, another set of specimens is austenitized singly in the temperature range 1150 - 1050 degrees C. Tempering process was carried out between 500 - 640 degrees ...
THE INFLUENCE OF MANUFACTURING DEFECTS ON STRUCTURAL PERFORMANCE OF COMPOSITE OVERWRAPPED PRESSURE VESSELS
Yurdakul, Kıvanç; Gürbüz, Rıza; Department of Metallurgical and Materials Engineering (2022-2-04)
In this study, the influence of defects that are occurred in manufacturing operations of filament wound composite overwrapped pressure vessels on burst pressure is investigated experimentally. Firstly, material characterization methods such as tensile testing and fiber volume fraction testing of carbon/epoxy composite specimens are completed. Following determining of different layer configurations for small scale composite pressure vessels, manufacturing and burst testing of vessels are accomplished. Ef...
Effect of microstructural modification on damage tolerance of 34CrMo4 shaft steel
Ozcan, Burak; Gurer, Goksu; Gür, Cemil Hakan (Wiley, 2020-06-01)
Overall damage tolerances of the heat-treated 34CrMo4 steels having ferritic-pearlitic, bainitic, and tempered-martensitic microstructures were evaluated based on their threshold stress intensity factor prior to small crack propagation, fatigue strength, and fracture toughness under static loading. Kitagawa-Takahashi diagrams were constructed to determine the limiting size of small crack propagation. The micromechanical effects of carbide morphology and phase distribution on quasi-static and dynamic mechani...
The effect of austempering parameters on impact and fracture toughness of din 35nicrmov12.5 gun barrel steel
Aksu, Engin; Atala, Haluk; Department of Metallurgical and Materials Engineering (2005)
In this study the effects of different austempering times and temperatures on impact toughness, hardness and fracture toughness properties of 35NiCrMoV12.5 gun barrel steel are investigated. 300 °C, 325 °C and 350 °C were chosen as austempering temperatures. Isothermal holding times at these temperatures were chosen as 1 minute, 10 minutes, 1 hour and 10 hours. It was found that, 350 °C being an exception, austempering temperature and impact toughness has an inverse relationship and impact toughness increas...
The effect of SN content and isothermal transformation temperature on the mechanical properties of austempered ductile cast iron
Özcan, Alper; Atala, Haluk; Department of Metallurgical and Materials Engineering (2003)
In this study the effects of Sn content and isothermal transformation temperature on the ultimate tensile strength (UTS), elongation and hardness of austempered ductile cast iron (ADI) was investigated. To determine the possible effect of Sn on these properties the Sn content of standard GGG30, GGG40 and GGG50 materials were taken as reference, whose chemical compositions vary from 0,016 to 0,050% in terms of Sn. However the Sn content was increased to a maximum of 0,26% for investigating the effect of Sn o...
Citation Formats
IEEE
ACM
APA
CHICAGO
MLA
BibTeX
A. Ozturk, “The influence of cyclic fatigue damage on the fracture toughness of carbon-carbon composites,”
COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING
, pp. 641–646, 1996, Accessed: 00, 2020. [Online]. Available: https://hdl.handle.net/11511/64150.