Find the “raw” endurance strength, Se’
For
steel, use:
Bending: Se’ = 0.50 Sut
up to a max of 100 ksi
Axial: Se’
= 0.45 Sut up to a max of 90 ksi (Eqn.
7.7)
Torsion: Se’ = 0.29 Sut up
to a max of 58 ksi
This is Se’ for a polished
0.3” diameter bar.
D erate Se’ to represent your application.
kf
Surface effect – if not polished
ks Size effect – if not < 0.3” diameter
kr Reliability effect – if other than 50% survival
kt Temperature effect – if not at Room Temperature
km Miscellaneous – Mat’l processing, Residual stress, Coatings, Corrosion
Se = kf ks kr kt km Se’
(My
Part) (Test Specimen)
3) Account for Stress Concentration with Notch Sensitivity
Compute
Kf = 1 + (Kc –1)qn and either
divide Se by Kf or multiply your actual
alternating stress alt
by Kf.
4)
Find the fatigue strength at the 1000 cycle Low Cycle Fatigue point,
SL’
For
steel, use:
Bending: SL’ = 0.90 Sut
Axial: SL’
= 0.75 Sut (Eqn. 7.8)
Torsion: SL’
= 0.72 Sut
5)
Build the S-N Curve
On
Linear-Log paper, put:
Sut at 1 cycle (Because it can endure 1 cycle to Sut)
SL’ at 1000 cycles
Se (derated for your part) at 106 cycles and beyond
C
onnect
(1000, SL’) and (106, Se)
with the curve
,
where
and
N = Number of cycles.
I f you have a or c and b , and want to know the life for an alternating stress alt between Se and SL’, compute
Chart
from FatigueH.xls
Chart
from FatigueH.xls
ALL INFORMATION IN THIS RISK ASSESSMENT MUST BE FULLY
ANNEX A1 DMHAS ASAM SERVICE DESCRIPTIONS PLEASE CAREFULLY REVIEW
APPLICATION FOR EMPLOYMENT (PLEASE COMPLETE FULLY IN BLACK INK)
Tags: fatigue procedure, cycle fatigue, fully, fatigue, procedure, reversing, “raw”