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

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

Funding

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