Titanium matrix composite durability analyses for the design of airframe structures
Conference
·
OSTI ID:536401
- McDonnell Douglas Aerospace, St. Louis, MO (United States)
- Wright Labs., Wright Patterson AFB, OH (United States)
A fatigue life prediction technique is described for use with titanium matrix composite materials. Damage modes specific to this material system are discussed for unnotched and center-notched laminates. Test data for isothermal fatigue and thermomechanical fatigue specimens are compared against predictions made using the analysis method.
- OSTI ID:
- 536401
- Report Number(s):
- CONF-940399--; ISBN 0-8031-2039-7
- Country of Publication:
- United States
- Language:
- English
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