Time-Resolved Particle Image Velocimetry (TR-PIV) was used to study the vortical structures resulting from a submerged water jet impinging normally on a smooth and flat surface. A fully developed turbulent jet, exiting a long pipe, and a semi-confined flow configuration ensured properly characterized boundary conditions, which allows for straightforward assessment of turbulence models and numerical schemes. The Reynolds number based on jet mean exit velocity was 23,000. The pipe-to-plate separation was varied between 2D and 7.6D. Turbulent velocity fields are presented using Reynolds decomposition into mean and fluctuating components. Proper Orthogonal Decomposition (POD) analysis was used to identify the most energetic coherent structures of the turbulent flow field. Three velocity gradient-based vortex identification techniques, 2nd invariant Q, λ2, and swirling strength, were found to perform equally well in identifying vortical structures along the impingement wall. The results clearly demonstrate the shortcomings of local vorticity as a vortex identifier in an impinging jet flow field.
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ASME 2009 International Mechanical Engineering Congress and Exposition
November 13–19, 2009
Lake Buena Vista, Florida, USA
Conference Sponsors:
- ASME
ISBN:
978-0-7918-4382-6
PROCEEDINGS PAPER
A Time-Resolved PIV Study of Vortical Structures in the Near-Wall Region of an Impinging Round Jet
Khaled J. Hammad,
Khaled J. Hammad
Dantec Dynamics Inc., Ramsey, NJ
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Ivana M. Milanovic
Ivana M. Milanovic
University of Hartford, West Hartford, CT
Search for other works by this author on:
Khaled J. Hammad
Dantec Dynamics Inc., Ramsey, NJ
Ivana M. Milanovic
University of Hartford, West Hartford, CT
Paper No:
IMECE2009-13076, pp. 371-381; 11 pages
Published Online:
July 8, 2010
Citation
Hammad, KJ, & Milanovic, IM. "A Time-Resolved PIV Study of Vortical Structures in the Near-Wall Region of an Impinging Round Jet." Proceedings of the ASME 2009 International Mechanical Engineering Congress and Exposition. Volume 9: Heat Transfer, Fluid Flows, and Thermal Systems, Parts A, B and C. Lake Buena Vista, Florida, USA. November 13–19, 2009. pp. 371-381. ASME. https://doi.org/10.1115/IMECE2009-13076
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