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

Project: Research project

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
StatusFinished
Effective start/end date9/1/189/15/20

Funding

  • DOD-NAVY: Naval Air Systems Command (NAVAIR): $210,000.00

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