This study is devoted to a forced turbulent plane jet emerging from a slot rectangular nozzle impinging on a semi-cylindrical surface using large eddy simulation. Both forced and unforced cases are considered. The Reynolds number, based on the slot velocity and width, was 5600. The LES simulations were validated using published experimental results and contrasted against RANS models. The study is performed for a slot-to-surface distance equal to twice the nozzle width and considers two forcing frequencies equal to 400 and 800 Hz. The jet was excited using a sinusoidal inlet velocity profile at several harmonics of the preferred mode and the flow and heat transfer characteristics were analyzed. The phase averaged Nusselt number exhibited several peaks along the semi-circular target plane. Increases above the steady unforced jet values of heat transfer rates were obtained in the stagnation region and decreases were observed in the wall jet region. The fluctuations in the phase averaged surface Nusselt number are explained in terms of the interaction of organized shear layer structures with induced target wall structures.
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ASME 2013 Fluids Engineering Division Summer Meeting
July 7–11, 2013
Incline Village, Nevada, USA
Conference Sponsors:
- Fluids Engineering Division
ISBN:
978-0-7918-5554-6
PROCEEDINGS PAPER
Large Eddy Simulation of a Forced Turbulent Jet Impacting on a Semi-Cylinder
L. Khezzar,
L. Khezzar
The Petroleum Institute, Abu Dhabi, UAE
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N. Kharoua
N. Kharoua
The Petroleum Institute, Abu Dhabi, UAE
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Z. Li
The Petroleum Institute, Abu Dhabi, UAE
L. Khezzar
The Petroleum Institute, Abu Dhabi, UAE
N. Kharoua
The Petroleum Institute, Abu Dhabi, UAE
Paper No:
FEDSM2013-16321, V01AT03A013; 7 pages
Published Online:
December 13, 2013
Citation
Li, Z, Khezzar, L, & Kharoua, N. "Large Eddy Simulation of a Forced Turbulent Jet Impacting on a Semi-Cylinder." Proceedings of the ASME 2013 Fluids Engineering Division Summer Meeting. Volume 1A, Symposia: Advances in Fluids Engineering Education; Advances in Numerical Modeling for Turbomachinery Flow Optimization; Applications in CFD; Bio-Inspired Fluid Mechanics; CFD Verification and Validation; Development and Applications of Immersed Boundary Methods; DNS, LES, and Hybrid RANS/LES Methods. Incline Village, Nevada, USA. July 7–11, 2013. V01AT03A013. ASME. https://doi.org/10.1115/FEDSM2013-16321
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