THROUGH-THE-THICKNESS FATIGUE CRACK CLOSURE BEHAVIOR IN AN ALUMINUM ALLOY

THROUGH-THE-THICKNESS FATIGUE CRACK CLOSURE BEHAVIOR IN AN ALUMINUM ALLOY

Author(s):

Publication title:

NASA Technical Reports

Pub. Year:

1990

Issue:

NASA-TM-102590

No.:

G3/39 0271145

Pt.:

NAS 1.15:102590

Paper no.:

N90-20427

Page(from):

1

Page(to):

8

Pages:

8

Pub. info.:

National Aeronautics and Space Adminstration

Language:

English

Type:

Technical Paper

Details

TDL ID:

ZA00001426

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