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A PROCEDURE FOR UTILIZATION OF A DAMAGE-DEPENDENT CONSTITUTIVE MODEL FOR LAMINATED COMPOSITES

Author(s):
Publication title:
NASA Technical Reports
Pub. Year:
1992
Issue:
NASA-TM-104219
Pt.:
NAS 1.15:104219
Paper no.:
N92-25135
Page(from):
1
Page(to):
32
Pages:
32
Pub. info.:
National Aeronautics and Space Adminstration
Language:
English
Type:
Technical Paper

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