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TECHNICAL PAPERS

Separated Flow Transition Under Simulated Low-Pressure Turbine Airfoil Conditions—Part 2: Turbulence Spectra

[+] Author and Article Information
Ralph J. Volino

Department of Mechanical Engineering, United States Naval Academy, Annapolis, MD 21402e-mail: volino@usna.edu

J. Turbomach 124(4), 656-664 (Nov 07, 2002) (9 pages) doi:10.1115/1.1506939 History: Received January 22, 2002; Online November 07, 2002
Copyright © 2002 by ASME
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References

Figures

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Contours of f⋅PSD(u′2)/U2, low FSTI cases; station number indicated above each column; by row—(a) Re=25,000, (b) Re=50,000, (c) Re=100,000, (d) Re=200,000, (e) Re=300,000; outer contour magnitude and contour spacing indicated by numerical value in field of each subplot, 5 contours shown in each subplot
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Spectra of f⋅PSD(u′2)/U2, low FSTI, Re=100,000, Station 10
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Contours of f⋅PSD(−uv)/U2, low FSTI cases; see Fig. 5 caption for further explanation
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Contours of f⋅PSD(u′2)/U2, high FSTI cases; see Fig. 5 caption for further explanation
Grahic Jump Location
Spectra of f⋅PSD(u′2)/U2, high FSTI, Re=100,000, Station 10
Grahic Jump Location
Contours of f⋅PSD(−uv)/U2, high FSTI cases; see Fig. 5 caption for further explanation
Grahic Jump Location
Contours of fPSD(u′2), high FSTI, Re=300,000, Station 4; outer contour magnitude and contour spacing indicated by numerical value in field of figure
Grahic Jump Location
Contours of fPSD(u′2), low FSTI, Re=100,000, Station 4; outer contour magnitude and contour spacing indicated by numerical value in field of figure
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Free-stream spectra for high FSTI, Re=300,000 case—(a) u, (b) v
Grahic Jump Location
Free-stream spectra for low FSTI, Re=300,000 case—(a) u, (b) v

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