SYMPOSIA PAPER Published: 01 January 1990
STP24106S

Certification Testing Methodology for Fighter Hybrid Structure

Source

A methodology for certification testing of bolted hybrid aircraft structures was developed that accounts for inherent differences between composite and metal behavior. The effects of scatter and environment on static strength and fatigue life certification were characterized based on analytic correlation with test results of over 8000 carbon/epoxy specimens.

Author Information

Sanger, KB
McDonnell Aircraft Co., McDonnell Douglas Corp., St. Louis, MO
Dill, HD
McDonnell Aircraft Co., McDonnell Douglas Corp., St. Louis, MO
Kautz, EF
Naval Air Development Center, Warminster, PA
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Details
Developed by Committee: D30
Pages: 34–47
DOI: 10.1520/STP24106S
ISBN-EB: 978-0-8031-5120-8
ISBN-13: 978-0-8031-1287-2