Now showing items 1-2 of 2
Physics based prediction of aeromechanical loads for the UH-60A rotor
(Georgia Institute of Technology, 2013-04-12)
Helicopters in forward flight experience complex aerodynamic phenomena to various degrees. In low speed level flight, the vortex wake remains close to the rotor disk and interacts with the rotor blades to give rise to blade ...
A matched-harmonic confluence approach to rotor loads prediction with comprehensive application to flight test
(Georgia Institute of Technology, 2012-09-18)
Future management of helicopter fleets will be more heavily based on individual component damage tracking and less on legacy usage monitoring (flight parameter-based) methods. This enhances health assessment capabilities ...