The development of a wake flow downstream of a cylindrical rod within a curved channel under zero streamwise pressure gradient is theoretically and experimentally investigated. The measured asymmetric wake quantities such as the mean velocity and turbulent fluctuations in longitudinal and lateral directions as well as the turbulent shear stress are transformed from the probe coordinate system into the curvilinear wake eigen-coordinate system. For the transformed non-dimensionalized velocity defect and the turbulent quantities, affine profiles are observed throughout the flow regime. Based on these observations and using the transformed equations of motion and continuity, a theoretical frame work is established that generally describes the two-dimensional curvilinear wake flow. The theory also describes the straight wake as a special case, for which the curvature radius approaches infinity. The comparison of the theory with the experimental data pertaining to the curvilinear and straight wakes demonstrate the general validity of the theory.
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ASME 1994 International Gas Turbine and Aeroengine Congress and Exposition
June 13–16, 1994
The Hague, Netherlands
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-7883-5
PROCEEDINGS PAPER
Development of Two-Dimensional Wakes Within Curved Channels, Theoretical Framework and Experimental Investigation Free
M. T. Schobeiri,
M. T. Schobeiri
Texas A&M University, College Station, TX
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J. John,
J. John
Texas A&M University, College Station, TX
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K. Pappu
K. Pappu
Texas A&M University, College Station, TX
Search for other works by this author on:
M. T. Schobeiri
Texas A&M University, College Station, TX
J. John
Texas A&M University, College Station, TX
K. Pappu
Texas A&M University, College Station, TX
Paper No:
94-GT-367, V001T01A127; 15 pages
Published Online:
February 18, 2015
Citation
Schobeiri, MT, John, J, & Pappu, K. "Development of Two-Dimensional Wakes Within Curved Channels, Theoretical Framework and Experimental Investigation." Proceedings of the ASME 1994 International Gas Turbine and Aeroengine Congress and Exposition. Volume 1: Turbomachinery. The Hague, Netherlands. June 13–16, 1994. V001T01A127. ASME. https://doi.org/10.1115/94-GT-367
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