Experimental results are presented to document hydrodynamic and thermal development of flat-plate boundary layers undergoing natural transition. Local heat transfer coefficients, skin friction coefficients, and profiles of velocity, temperature, and Reynolds normal and shear stresses are presented. A case with no transition and transitional cases with 0.68 percent and 2.0 percent free-stream disturbance intensities were investigated. The locations of transition are consistent with earlier data. A late-laminar state with significant levels of turbulence is documented. In late-transitional and early-turbulent flows, turbulent Prandtl number and conduction layer thickness values exceed, and the Reynolds analogy factor is less than, values previously measured in fully turbulent flows.
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October 1985
Research Papers
Heat Transfer and Fluid Mechanics Measurements in Transitional Boundary Layer Flows
T. Wang,
T. Wang
Department of Mechanical Engineering, Clemson University, Clemson, S.C.
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T. W. Simon,
T. W. Simon
Department of Mechanical Engineering, University of Minnesota, Minneapolis, Minn.
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J. Buddhavarapu
J. Buddhavarapu
TSI, Inc., St. Paul, Minn.
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T. Wang
Department of Mechanical Engineering, Clemson University, Clemson, S.C.
T. W. Simon
Department of Mechanical Engineering, University of Minnesota, Minneapolis, Minn.
J. Buddhavarapu
TSI, Inc., St. Paul, Minn.
J. Eng. Gas Turbines Power. Oct 1985, 107(4): 1007-1015 (9 pages)
Published Online: October 1, 1985
Article history
Received:
December 27, 1984
Online:
October 15, 2009
Citation
Wang, T., Simon, T. W., and Buddhavarapu, J. (October 1, 1985). "Heat Transfer and Fluid Mechanics Measurements in Transitional Boundary Layer Flows." ASME. J. Eng. Gas Turbines Power. October 1985; 107(4): 1007–1015. https://doi.org/10.1115/1.3239804
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