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Some computational tools for the analysis of through cracks in stiffened fuselage shells

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Publication:1313891
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DOI10.1007/BF00370132zbMath0800.73316OpenAlexW1975834838MaRDI QIDQ1313891

Francis A. Brogan, Charles C. Rankin, Eduard Riks

Publication date: 1 March 1994

Published in: Computational Mechanics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/bf00370132


Mathematics Subject Classification ID

Fracture and damage (74R99) Membranes (74K15)


Related Items

Crack growth modeling via 3D automatic adaptive mesh refinement based on modified-SPR technique, Postbuckling behavior and imperfection sensitivity of elastic structures by the Lyapunov-Schmidt-Koiter approach, A perturbation method for the determination of the buckling strength of imperfection-sensitive structures, On the solution of mode jumping phenomena in thin-walled shell structures, Stability of smooth and ribbed shells of revolution in a nonuniform stress-strain state. (Survey), The arbitrary local mesh replacement method: An alternative to remeshing for crack propagation analysis, Numerical simulation of delamination growth in curved interfaces


Uses Software

  • STAGS


Cites Work

  • On the method of virtual crack extensions
  • Unnamed Item
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