NASA/FLAGRO 2.0 developed as analytical aid in predicting growth and stability of preexisting flaws and cracks in structural components of aerospace systems. Used for fracture-control analysis of space hardware. Organized into three modules to maximize efficiency in operation. Useful in: (1) crack-instability/crack-growth analysis, (2) processing raw crack-growth data from laboratory tests, and (3) boundary-element analysis to determine stresses and stress-intensity factors. Written in FORTRAN 77 and ANSI C.
Updated Fatigue-Crack-Growth And Fracture-Mechanics Software
NASA Tech Briefs ; 19 , 12
1995-12-01
Miscellaneous
No indication
English
Updated Fatigue-Crack-Growth and Fracture-Mechanics Software
Online Contents | 1995
SOLUTIONS - Software - Advanced-Fatigue-Crack-Growth and Fracture-Mechanics Program
Online Contents | 2002
SAE Technical Papers | 2023
|