Progressive Damage Analysis of Laminated Composite (PDALC)-A Computational Model Implemented in the NASA COMET Finite Element Code

Progressive Damage Analysis of Laminated Composite (PDALC)-A Computational Model Implemented in the NASA COMET Finite Element Code

Author(s):

Publication title:

NASA Technical Reports

Pub. Year:

1996

Vol.:

19970002981

Issue:

NASA-TM-4724

Pt.:

NAS 1.15:4724

Page(from):

1

Page(to):

48

Pages:

48

Pub. info.:

National Aeronautics and Space Adminstration

Language:

English

Type:

Technical Paper

Details

TDL ID:

ZA00001434

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