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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

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Figures

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

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