Research Catalog

Fatigue life methodology for tapered composite flexbeam laminates

Title
Fatigue life methodology for tapered composite flexbeam laminates [microform] / Gretchen B. Murri, T. Kevin O'Brien, Carl Q. Rousseau.
Author
Murri, Gretchen B.
Publication
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]

Details

Additional Authors
  • O'Brien, T. Kevin.
  • Rousseau, Carl Q.
  • United States. National Aeronautics and Space Administration.
Description
1 v.
Series Statement
[NASA contractor report] ; NASA-CR-204524
Uniform Title
NASA contractor report ; NASA CR-204524.
Subject
  • Fatigue life
  • Finite element method
  • Laminates
  • Delaminating
  • Strain energy release rate
  • Cyclic loads
  • Glass fiber reinforced plastics
  • Epoxy matrix composites
  • Fatigue tests
Note
  • Shipping list no.: 98-0933-M.
Reproduction (note)
  • Microfiche.
Call Number
READEX Microfiche NAS 1.26:204524
OCLC
marcive42957898
Author
Murri, Gretchen B.
Title
Fatigue life methodology for tapered composite flexbeam laminates [microform] / Gretchen B. Murri, T. Kevin O'Brien, Carl Q. Rousseau.
Imprint
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
Series
[NASA contractor report] ; NASA-CR-204524
NASA contractor report ; NASA CR-204524.
Reproduction
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997] 1 microfiche.
Added Author
O'Brien, T. Kevin.
Rousseau, Carl Q.
United States. National Aeronautics and Space Administration.
Gpo Item No.
0830-H-14 (MF)
Sudoc No.
NAS 1.26:204524
Research Call Number
READEX Microfiche NAS 1.26:204524
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