Delamination Behavior of Quasi-Isotropic Graphite Epoxy Laminates Subjected to Tension and Torsion Loads

Delamination Behavior of Quasi-Isotropic Graphite Epoxy Laminates Subjected to Tension and Torsion Loads

Author(s):

Hinkley, J.A. ( NASA Langley Research Center and Aerostructures Directorate )
O'Brien, T.K.

Publication title:

NASA Technical Reports

Pub. Year:

1992

Issue:

NASA-TM-104181

Pt.:

NAS 1.15:104181

Paper no.:

N92-22624

Page(from):

1

Page(to):

17

Pages:

17

Pub. info.:

National Aeronautics and Space Adminstration

Language:

English

Type:

Technical Paper

Details

TDL ID:

ZA00001428

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