CONTACT   |   FAQS   |   SITE DIRECTORY   |   TERMS OF USE   |   HOME 
CHOOSE FROM A TOOL BELOW:
Home Page

Stress Life Calculations
Strain Life Calculations
Stress-Strain Plotting
Power Law Fit/Regression Analysis
Linear Elastic Fracture Mechanics
Notches with Stress Life
Notches with Strain Life
Multi-axial Fatigue Analysis
Variable Amplitude Analysis (future)
Author Change Log
Leave Feedback for the author
References

Compute number of cycles to failure (Foremans's Equation)


Nf =     af

ai  
   (1-R)Kc-ΔK    da
C(ΔK)m
Center-cracked Plate
Edge-cracked plate Double-edge cracked Plate
Cracked-beam in pure bending Circular Crack in Infinite Body
Semi-Circular Crack in Thick Plate Circular Corner Crack in Thick Plate
Initial Crack, ai
Final Crack, af
Stress Ratio, R
Paris's Eqn. Material Constant,C
Paris's Eqn. Material Constant(3 to 4), m
Applied Stress, Δσ
Maximum Stress, σmax
Stress Intensity, Kc




Use of this site signifies your agreement to the terms of use.
© Cricelli, Inc. 2009 All rights reserved.