Physics based prediction of aeromechanical loads for the UH-60A rotor

Physics based prediction of aeromechanical loads for the UH-60A rotor

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 vortex interaction phenomena. In high speed flight, compressibility effects...

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Bibliographic Details
Main Author: Marpu, Ritu Priyanka
Published: Georgia Institute of Technology 2013
Subjects:
CFD
UH-60A
Maneuver
Helicopter
Rotorcraft CFD/CSD
Rotors (Helicopters)
Rotors Dynamics
Aerodynamic load
Aerodynamics
Computational fluid dynamics
Online Access:http://hdl.handle.net/1853/47661

Internet

http://hdl.handle.net/1853/47661

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