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TECHNICAL PAPERS

Effect of Two-Scale Roughness on Boundary Layer Transition Over a Heated Flat Plate: Part 2—Boundary Layer Structure

[+] Author and Article Information
Mark W. Pinson, Ting Wang

Department of Mechanical Engineering, Clemson University, Clemson, SC 29634-0921

J. Turbomach 122(2), 308-316 (Feb 01, 1999) (9 pages) doi:10.1115/1.555454 History: Received February 01, 1999
Copyright © 2000 by ASME
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References

Figures

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Comparisons with intermittency models: (a) with Narasimha intermittency distributions; (b) and (c) with Mayle’s smooth-wall correlations. Data from Refs. 2829303132.
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Skin-friction distributions and Reynolds analogy factor Grahic Jump Location
Selected normalized velocity profiles: (a) baseline; (b) 100/100
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Selected distributions of turbulent quantities for baseline case at 16.1 m/s
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Selected distributions of turbulent quantities for 100/100 case at 8.6 m/s
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Streamwise development of peak turbulent quantities in the boundary layer
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Power spectral density: (a) baseline, 16.1 m/s; (b) STEP/100, 4.6 m/s
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Selected power spectral distributions: (a) baseline, 16.1 m/s; (b) 60/0, 8.6 m/s; (c) 60/100, 8/6 m/s; (d) STEP/100; (e) 100/100, 8.6 m/s
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Selected results of wavelet transformations of baseline data using Morlet wavelet function
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Selected results of wavelet transformations using Morlet wavelet function: (a) 60/0 case; (b) 100/100 case

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