Research Catalog

Fatigue life methodology for tapered composite flexbeam laminates

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

Details

Additional Authors
  • O'Brien, T. Kevin.
  • Rousseau, Carl Q.
  • Langley Research Center.
Description
1 v.
Series Statement
NASA technical memorandum ; 112860
Subject
  • Strain energy release rate
  • Finite element method
  • Laminates
  • Delaminating
  • Fatigue life
  • Fatigue (Materials)
  • Glass fiber reinforced plastics
  • Rotary wings
Note
  • Shipping list no.: 98-0818-M.
Reproduction (note)
  • Microfiche.
Call Number
READEX Microfiche NAS 1.15:112860
OCLC
marcive39783311
Author
Murri, Gretchen B.
Title
Fatigue life methodology for tapered composite flexbeam laminates [microform] / Gretchen B. Murri and T. Kevin O'Brien, Carl Q. Rousseau.
Imprint
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
Series
NASA technical memorandum ; 112860
Reproduction
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997] 1 microfiche.
Added Author
O'Brien, T. Kevin.
Rousseau, Carl Q.
Langley Research Center.
Gpo Item No.
0830-D (MF)
Sudoc No.
NAS 1.15:112860
Research Call Number
READEX Microfiche NAS 1.15:112860
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