Research Catalog

Three-dimensional elastic-plastic finite-element analysis of fatigue crack propagation

Title
Three-dimensional elastic-plastic finite-element analysis of fatigue crack propagation [microform] / by R.G. Chermahini and G.L. Goglia.
Author
Chermahini, R. G.
Publication
Norfolk, Va. : Old Dominion University Research Foundation, [1985]

Details

Additional Authors
  • Goglia, G. L.
  • Old Dominion University. Department of Mechanical Engineering and Mechanics.
  • Langley Research Center.
Description
1 v.
Series Statement
NASA CR ; 176415
Uniform Title
NASA contractor report ; NASA CR-176415.
Subject
  • Aircraft structures
  • Crack propagation
  • Cracks
  • Fatigue (materials)
  • Finite element method
Note
  • "Final report for the period June 1, 1985 to November 1, 1985."
  • "Prepared for National Aeronautics and Space Administration Langley Research Center, under Research Grant NAG-1-529."
  • "November 1985."
Bibliography (note)
  • Includes bibliographical references.
Reproduction (note)
  • Microfiche.
Call Number
GPO Microfiche NAS 1.26:176415
OCLC
marcive476752011
Author
Chermahini, R. G.
Title
Three-dimensional elastic-plastic finite-element analysis of fatigue crack propagation [microform] / by R.G. Chermahini and G.L. Goglia.
Imprint
Norfolk, Va. : Old Dominion University Research Foundation, [1985]
Series
NASA CR ; 176415
NASA contractor report ; NASA CR-176415.
Bibliography
Includes bibliographical references.
Reproduction
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration]. 1986. 1 microfiche.
Added Author
Goglia, G. L.
Old Dominion University. Department of Mechanical Engineering and Mechanics.
Langley Research Center.
Other Form:
Paper version: Chermahini, R. G. Three-dimensional elastic-plastic finite-element analysis of fatigue crack propagation. (OCoLC)16859447
Online version: Chermahini, R. G. Three-dimensional elastic-plastic finite-element analysis of fatigue crack propagation. (OCoLC)476753730
Gpo Item No.
0830-H-14 (MF)
Sudoc No.
NAS 1.26:176415
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