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

Project: Research project

Project Details

Description

GUIde 4 Consortium: Unsteady Aerodynamics and Aeromechanics Methods: Entire Blade Disk Damping Through Dampers on Only a Few Blades - Fail-Safe Optimi GUIde Consortium: Entire Blade Disk Damping Through Dampers on Only a Few Blades - Fail-Safe Optimization
StatusFinished
Effective start/end date9/2/0911/7/13

Funding

  • DOD-USAF: Air Force Research Labs (AFRL): $131,538.00

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