Correction: CFD study on NACA 4415 airfoil implementing spherical and sinusoidal Tubercle Leading Edge
Autor: | Kamarul Arifin Ahmad, Syed Mohammed Aminuddin Aftab |
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Jazyk: | angličtina |
Rok vydání: | 2017 |
Předmět: |
Velocity
Marine and Aquatic Sciences lcsh:Medicine 02 engineering and technology Leading Edges 0202 electrical engineering electronic engineering information engineering lcsh:Science Mammals Multidisciplinary Physics 05 social sciences Classical Mechanics Mechanics Drag NACA airfoil Data Acquisition NACA Humpback Whales Physical Sciences Vertebrates Engineering and Technology Bubbles 020201 artificial intelligence & image processing Geology Research Article Airfoil Computer and Information Sciences Leading edge Reynolds Number Tubercle Aerospace Engineering Marine Biology Fluid Mechanics Computational fluid dynamics Continuum Mechanics Motion 0502 economics and business Animals Marine Mammals 050210 logistics & transportation business.industry lcsh:R Organisms Whales Biology and Life Sciences Fluid Dynamics Turbulence Amniotes Earth Sciences lcsh:Q business |
Zdroj: | PLoS ONE, Vol 12, Iss 11, p e0188792 (2017) PLoS ONE |
ISSN: | 1932-6203 |
Popis: | The Humpback whale tubercles have been studied for more than a decade. Tubercle Leading Edge (TLE) effectively reduces the separation bubble size and helps in delaying stall. They are very effective in case of low Reynolds number flows. The current Computational Fluid Dynamics (CFD) study is on NACA 4415 airfoil, at a Reynolds number 120,000. Two TLE shapes are tested on NACA 4415 airfoil. The tubercle designs implemented on the airfoil are sinusoidal and spherical. A parametric study is also carried out considering three amplitudes (0.025c, 0.05c and 0.075c), the wavelength (0.25c) is fixed. Structured mesh is utilized to generate grid and Transition SST turbulence model is used to capture the flow physics. Results clearly show spherical tubercles outperform sinusoidal tubercles. Furthermore experimental study considering spherical TLE is carried out at Reynolds number 200,000. The experimental results show that spherical TLE improve performance compared to clean airfoil. |
Databáze: | OpenAIRE |
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