Engineering PapersโŒ• Search

NASA NTRS ยท 19860000149

Fatigue-Crack-Growth Structural Analysis

Abstract

Elastic and plastic deformations calculated under variety of loading conditions. Prediction of fatigue-crack-growth lives made with FatigueCrack-Growth Structural Analysis (FASTRAN) computer program. As cyclic loads are applied to initial crack configuration, FASTRAN predicts crack length and other parameters until complete break occurs. Loads are tensile or compressive and of variable or constant amplitude. FASTRAN incorporates linear-elastic fracture mechanics with modifications of load-interaction effects caused by crack closure. FASTRAN considered research tool, because of lengthy calculation times. FASTRAN written in FORTRAN IV for batch execution.

Keep this discovery

Explore connections, maps & timelines

BibTeXRIS

Newman, J. C., Jr.. 1986-05-01. Fatigue-Crack-Growth Structural Analysis. https://ntrs.nasa.gov/citations/19860000149

Cite the original work for its findings. Save a collection to share your selection of sources.