Experimentally validated multi-step simulation strategy to predict the fatigue crack propagation rate in residual stress fields after laser shock peening
Publikation: Beiträge in Zeitschriften › Zeitschriftenaufsätze › Forschung › begutachtet
Standard
in: International Journal of Fatigue, Jahrgang 124, 01.07.2019, S. 265-276.
Publikation: Beiträge in Zeitschriften › Zeitschriftenaufsätze › Forschung › begutachtet
Harvard
APA
Vancouver
Bibtex
}
RIS
TY - JOUR
T1 - Experimentally validated multi-step simulation strategy to predict the fatigue crack propagation rate in residual stress fields after laser shock peening
AU - Keller, S.
AU - Horstmann, M.
AU - Kashaev, N.
AU - Klusemann, B.
PY - 2019/7/1
Y1 - 2019/7/1
N2 - Laser shock peening (LSP) is a promising technology to retard the fatigue crack propagation (FCP) in metallic lightweight structures. A multi-step simulation strategy to predict FCP in LSP-induced residual stress fields is proposed and applied. The simulation strategy involves an LSP process simulation, a transfer approach to include the plastic strains in a C(T) specimen model to calculate the residual stresses and an FCP simulation to determine the stress intensity factors. The FCP rate is finally determined via FCP equations. The validity of the simulation strategy including the crack driving quantities prediction is experimentally demonstrated by a novel ‘simulation’ approach.
AB - Laser shock peening (LSP) is a promising technology to retard the fatigue crack propagation (FCP) in metallic lightweight structures. A multi-step simulation strategy to predict FCP in LSP-induced residual stress fields is proposed and applied. The simulation strategy involves an LSP process simulation, a transfer approach to include the plastic strains in a C(T) specimen model to calculate the residual stresses and an FCP simulation to determine the stress intensity factors. The FCP rate is finally determined via FCP equations. The validity of the simulation strategy including the crack driving quantities prediction is experimentally demonstrated by a novel ‘simulation’ approach.
KW - Engineering
KW - Fatigue crack growth
KW - Laser shock peening
KW - Numerical simulation
KW - Residual stresses
KW - Stress intensity factor
UR - http://www.scopus.com/inward/record.url?scp=85062706258&partnerID=8YFLogxK
U2 - 10.1016/j.ijfatigue.2018.12.014
DO - 10.1016/j.ijfatigue.2018.12.014
M3 - Journal articles
AN - SCOPUS:85062706258
VL - 124
SP - 265
EP - 276
JO - International Journal of Fatigue
JF - International Journal of Fatigue
SN - 0142-1123
ER -