Active Control of Turbulent Boundary Layers for Drag and Noise Reduction in Naval Applications
Abstract
Lorentz Force actuators were developed and characterized. They were used to measure the effect of lorentz force control on the drag of a fully turbulent channel flow. Approximately 15% drag reduction was achieved
Document Details
- Document Type
- Technical Report
- Publication Date
- Jan 01, 2005
- Accession Number
- ADA432725
Entities
People
- Kenneth S. Breuer
Organizations
- Brown University