VFATIGUE

Vibration Fatigue Data

Description: Defines data needed for vibration fatigue analysis.

Format:

Example:

Field	Definition	Type	Default
SID	Set identification number.	Integer > 0	Required
APRCH	Fatigue life approach, one of the following character variables: STRESS or STRAIN.	Character	See Remark 2
METHOD	Life calculation method, selected by one of the following values 1 = von Mises stress/strain 2 = Maximum principal stress/strain 3 = Maximum shear stress/strain	Integer	2
DT	Event duration used to determine life. See Remark 5.	Real > 0.0	Required
TCF	Factor to convert DT and life output to units other than seconds. See Remark 5.	Real > 0.0	1.0
B	S-N curve slope. See Remark 3.	Real > 0.0	See Remark 2
SU	Intercept stress level. Typically taken as the material ultimate stress. See Remark 3.	Real > 0.0	See Remark 2
N0	Intercept cycles. See Remark 3.	Integer > 0	1000
KF	Factor applied to compensate for life reduction effects such as finish, corrosion, and notch effects. See Remark 3.	Real > 0.0	1.0
BE	Slope after endurance limit. See Remark 3.	Real > 0.0	0.1*B
SE	Endurance limit. See Remark 3.	Real ≥ 0.0	0.2*SU
SF	Coefficient of fatigue strength. See Remark 4.	Real > 0.0	See Remark 2
EF	Coefficient of fatigue ductility. See Remark 4.	Real > 0.0	See Remark 2
B	Exponent of fatigue strength. See Remark 4.	Real > 0.0	See Remark 2
C	Exponent of fatigue ductility. See Remark 4.	Real > 0.0	See Remark 2

Remarks:

1. VFATIGUE entries must all have unique set identification numbers.
2. The APRCH field is required when neither the SNDATA nor ENDATA Bulk Data entries are included. The data provided on the continuation entries serve as default values for properties normally defined on these entries. Values not specified on SNDATA entries will be replaced with ones from the STRESS continuation, and values not specified on the ENDATA will be replaced with ones from the STRAIN continuation.
3. The S-N curve shown in Figure 1 is characterized by the following equations:

   If

   

   If

   

   where,

   is the number of cycles to failure

   is the amplitude of input stress

   is the number of failure cycles at the endurance limit

   and the slope B shown in Figure 1 is calculated by:

   

4. The curve shown in Figure 2 is characterized by the equation:

   

   where,

   is the range of strain ( - )

   is the number of cycles to failure

   is the modulus of elasticity

5. The default value for DT is determined using the difference between the largest and smallest TABLEDi times (time range). If the specified DT is smaller that this time range, it is set equal to it. DT is useful when the event duration is different from the time range due to idling time. TCF is a time conversion factor that is typically used to convert a default DT time from seconds to another set of units such as hours. Life output will be in the same units as DT where life is defined using:

   

   where,

   Damage is the ratio of applied cycles over cycles to failure.

Figure 1. Stress-Life Curve Format

Figure 2. Strain-Life Curve Format