Now showing items 1-3 of 3
A multi-fidelity framework for physics based rotor blade simulation and optimization
(Georgia Institute of Technology, 2008-11-17)
New helicopter rotor designs are desired that offer increased efficiency, reduced vibration, and reduced noise. This problem is multidisciplinary, requiring knowledge of structural dynamics, aerodynamics, and aeroacoustics. ...
Computational fluid dynamic studies of high lift rotor systems using distributed computing
(Georgia Institute of Technology, 1995-05)
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 ...