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coating S-APPL
deposited O
by O
CS O
coating S-APPL
. O
The O
influence O
of O
AM S-MANP
and O
CS-induced O
residual B-PRO
stresses E-PRO
on O
fatigue S-PRO
performance O
of O
test O
specimens O
was O
thoroughly O
studied O
. O
Additionally O
, O
the O
effect O
of O
surface B-PRO
roughness E-PRO
and O
processes S-CONPRI
induced O
defects S-CONPRI
were O
considered O
to O
explain O
the O
crack B-CONPRI
growth E-CONPRI
mechanism O
. O
Stresses O
assessed O
by O
synchrotron S-ENAT
X-ray O
diffraction S-CHAR
indicated O
a O
substantial O
accumulation O
of O
the O
residual B-PRO
stresses E-PRO
, O
particularly O
in O
the O
outer O
surface S-CONPRI
of O
the O
as S-MATE
fabricated O
15-5 O
PH S-CONPRI
SS O
specimens O
. O
The O
state O
of O
residual B-PRO
stress E-PRO
was O
changed O
notably O
following O
the O
deposition S-CONPRI
of O
CrC-Ni O
coating S-APPL
in O
the O
axial O
, O
hoop O