NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Computer analysis of two-dimensional fatigue flaw-growth problemsA description is given of a computer program for analyzing the crack propagation in cyclic loaded structures. By using equations for the stress intensity factors for surface and embedded flaws, the capability of ascertaining lengthwise crack growth as well as crack growth through the thickness of the structure was determined. Equations used are written in general form so that many other types of crack growth problems, such as through the thickness type cracks, can be analyzed. Provisions have been made in the computer program to analyze crack growth for repeated blocks of variable-amplitude fatigue load spectra. Additional features of the computer program include a variable print interval and a variable integration interval to minimize computer printout and computer run time. A source listing and instructions for using the computer program are included.
Document ID
19720017287
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Forman, R. G.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Kavanaugh, H. C.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Stuckey, B.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Date Acquired
September 2, 2013
Publication Date
February 1, 1972
Subject Category
Structural Mechanics
Report/Patent Number
MSC-06006
NASA-TM-X-58086
Report Number: MSC-06006
Report Number: NASA-TM-X-58086
Accession Number
72N24937
Funding Number(s)
PROJECT: RTOP 908-42-38-00-72
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available