NASA NTRS · 19950008054
Study of multiple cracks in airplane fuselage by micromechanics and complex variables
Abstract
Innovative numerical techniques for two dimensional elastic and elastic-plastic multiple crack problems are presented using micromechanics concepts and complex variables. The simplicity and the accuracy of the proposed method will enable us to carry out the multiple-site fatigue crack propagation analyses for airplane fuselage by incorporating such features as the curvilinear crack path, plastic deformation, coalescence of cracks, etc.
Keep this discovery
Explore connections, maps & timelines
Denda, Mitsunori, Dong, Y. F.. 1994-09-01. Study of multiple cracks in airplane fuselage by micromechanics and complex variables. https://ntrs.nasa.gov/citations/19950008054
Cite the original work for its findings. Save a collection to share your selection of sources.