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ADDITIONAL TECHNICAL PAPERS

Loss Reduction Using Riblets on a Supersonic Through-Flow Fan Blade Cascade

[+] Author and Article Information
Todd Ninnemann, Wing F. Ng

Mechanical Engineering Department, Virginia Tech, MC 0238, Blacksburg, VA 24061

J. Fluids Eng 126(4), 642-649 (Sep 10, 2004) (8 pages) doi:10.1115/1.1667883 History: Received March 12, 2002; Revised October 30, 2003; Online September 10, 2004
Copyright © 2004 by ASME
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References

Figures

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Flow Field Description, Design Incidence
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Riblet Height Study (Shaded band is the trend based on previous studies)
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Measured Total Pressure Profiles Normalized by Upstream Total Pressure, Design Incidence
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Comparison of calculated skin friction coefficients, smooth blade versus simulated riblet effect (with no delayed transition)
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Comparison of calculated skin friction coefficients, smooth blade versus combined effect of riblet and delayed transition
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Comparison of calculated total pressure profiles, smooth blade versus combined effect of riblet and delayed transition

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