Title
A Polynomial Equation Model for Fatigue Crack Propagation in an Aeronautical Steel Material
Date Issued
01 January 2022
Access level
metadata only access
Resource Type
conference paper
Author(s)
Publisher(s)
Trans Tech Publications Ltd
Abstract
The model widely used in the fatigue crack growth study in materials science and fracture mechanics is the Paris-Erdogan, which relates the stress intensity factor with the subcritical crack growth, under a fatigue regime. In this work, a seven degree polynomial is used as an alternative to model the crack propagation behavior and to be able to analyze the three regions charts of the cycles by load, in contrast to the common model that it performs at a slight approximation of the propagation phase of the trinca (region II). Finally, a comparison has been made between the proposed model and the secant method by the ASTM 647,2000 standard that adjusts the points obtained experimentally. This proposed equation is new as another alternative analytical model for which the adjustment parameter “R” are compared in relation to the classical approach in a aeronautical ABNT 4130 steel.
Start page
212
End page
217
Volume
1053 MSF
Language
English
OCDE Knowledge area
Geología
Geociencias, Multidisciplinar
Subjects
DOI
Scopus EID
2-s2.0-85129424086
Source
Materials Science Forum
Resource of which it is part
Materials Science Forum
ISSN of the container
02555476
ISBN of the container
978-303572684-8
Conference
5th International Conference on Building Materials and Materials Engineering, ICBMM 2021 and 6th International Conference on Materials Technology and Applications, ICMTA 2021
Sources of information:
Directorio de Producción Científica
Scopus