Helicopter Blade Tip Vortex Modifications in Hover Using Piezoelectrically Modulated Blowing

Helicopter Blade Tip Vortex Modifications in Hover Using Piezoelectrically Modulated Blowing

Aeroacoustic investigations regarding different types of helicopter noise have indicated that the most annoying noise is caused by impulsive blade surface pressure changes in descent or forward flight conditions. Blade Vortex Interaction (BVI) is one of the main phenomena producing significant impu...

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Bibliographic Details
Main Author: Vasilescu, Roxana
Format: Others
Language:en_US
Published: Georgia Institute of Technology 2005
Subjects:
Piezoelectric actuation
Active flow control
CFD rotor wake
Rotor blade tip vortices
Unsteady modulated blowing
Rotors (Helicopters) Aerodynamics
Flutter (Aerodynamics)
Online Access:http://hdl.handle.net/1853/4896

Internet

http://hdl.handle.net/1853/4896

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