Project Details
Description
P-8A Aircraft Support for PMA-290 - Multiaxial Fatigue Crack Initiation and Growth Behavior of Al Alloys under Overloads and Underloads of Varying Biaxiality Ratios Multiaxial Fatigue Crack Initiation and Growth Behavior of Al Alloys under Overloads and Underloads of Varying Biaxiality Ratios
Status | Finished |
---|---|
Effective start/end date | 9/1/18 → 9/15/20 |
Funding
- DOD-NAVY: Naval Air Systems Command (NAVAIR): $210,000.00
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