Research Catalog

Experimental verification of a progressive damage model for IM7/5260 laminates subjected to tension-tension fatigue

Title
Experimental verification of a progressive damage model for IM7/5260 laminates subjected to tension-tension fatigue [microform] / Timothy W. Coats, Charles E. Harris.
Author
Coats, Timothy W.
Publication
[Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]

Details

Additional Authors
  • Harris, Charles E.
  • United States. National Aeronautics and Space Administration.
Description
1 v.
Series Statement
NASA-TM ; 111921
Uniform Title
NASA technical memorandum ; 111921.
Subject
  • Aircraft structures
  • Finite element method
  • Resin matrix composites
  • Crack propagation
  • Stiffness
  • Delaminating
  • Fiber composites
Note
  • Shipping list no.: 98-0599-M.
Reproduction (note)
  • Microfiche.
Call Number
READEX Microfiche NAS 1.15:111921
OCLC
marcive40426219
Author
Coats, Timothy W.
Title
Experimental verification of a progressive damage model for IM7/5260 laminates subjected to tension-tension fatigue [microform] / Timothy W. Coats, Charles E. Harris.
Imprint
[Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
Series
NASA-TM ; 111921
NASA technical memorandum ; 111921.
Reproduction
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997] 1 microfiche.
Added Author
Harris, Charles E.
United States. National Aeronautics and Space Administration.
Gpo Item No.
0830-D (MF)
Sudoc No.
NAS 1.15:111921
Research Call Number
READEX Microfiche NAS 1.15:111921
View in Legacy Catalog