GUIde 4 Consortium: Unsteady Aerodynamics Methods: Entire Blade Disk Damping Through Dampers on Only a Few Blades - Fail-Safe Optimization

Project: Research project

Project Details

StatusFinished
Effective start/end date9/2/0911/7/13

Funding

  • OTHER: Domestic Non-ABOR University: $75,239.00

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