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Experimental Investigation of the Flow Structure over a Delta Wing Via Flow Visualization Methods
Published on: April 23, 2018
Passive control of wing-tip vortices through a grooved-tip design
Junchen Tan1,2, Shūji Ōtomo3,4, Ignazio Maria Viola1
1School of Engineering, Institute for Energy Systems, University of Edinburgh, Edinburgh, EH9 3FB UK.
Novel grooved wing tips effectively control tip vortices, significantly reducing pressure drop by 40% with minimal impact on lift and drag. This passive flow control method enhances aerodynamic and hydrodynamic system efficiency.
Area of Science:
- Aerodynamics and Fluid Mechanics
- Hydrodynamics
- Vortex Dynamics
Background:
- Tip vortices generated by finite wings cause flow loss, noise, vibration, and cavitation.
- Effective control of tip vortices is crucial for improving efficiency in various wing- and blade-based systems.
Purpose of the Study:
- To investigate the characteristics and control of wing tip vortices using novel grooved-tip designs.
- To experimentally evaluate the impact of different grooved-tip configurations on tip vortex behavior and performance.
Main Methods:
- Utilized Particle Image Velocimetry (PIV) for streamwise and cross-flow measurements to visualize flow fields.
- Developed and tested four distinct grooved-tip designs, including tilted and shrinking grooves.
- Employed a reduced-order model to estimate pressure drop based on vortex swirling strength.
Main Results:
- Grooved-tip designs significantly reduced velocity magnitude and suction within the primary tip vortex core.
- Tip separation vortex was suppressed, and primary tip vortex strength was mitigated.
- Observed reduced vortex swirling strength, enlarged vortex dimensions, and an estimated 40% reduction in pressure drop.
Conclusions:
- Grooved-tip designs offer an effective passive strategy for modifying tip vortex behavior and mitigating pressure drop.
- These designs show potential for enhancing performance in hydrofoils, turbines, and propellers with negligible changes to lift and drag.
- The findings support the development of advanced passive vortex control strategies for marine and aerospace applications.
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