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ADDITIONAL TECHNICAL PAPERS

Detached-Eddy Simulations Over a Simplified Landing Gear

[+] Author and Article Information
L. S. Hedges

Boeing Commercial Airplanes, P.O. Box 3707, Seattle, WA 98124

A. K. Travin

Federal Scientific Center “Applied Chemistry,” St. Petersburg 197198, Russia

P. R. Spalart

Boeing Commercial Airplanes, P.O. Box 3707, Seattle, WA 98124e-mail: philippe.r.spalart@boeing.com

J. Fluids Eng 124(2), 413-423 (May 28, 2002) (11 pages) doi:10.1115/1.1471532 History: Received July 23, 2001; Revised January 24, 2002; Online May 28, 2002
Copyright © 2002 by ASME
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References

Figures

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Surface grids of the internal grid blocks
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Cp around the wheel when placed in the top view. (a) Front wheel; (b) rear wheel
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Cp around the wheel when placed in the side view. (a) Front wheel; (b) rear wheel
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Cp around the wheel when placed in the top view. (a) Front wheel; (b) rear wheel
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Pressure coefficient comparison on the front of the wheels
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Pressure coefficient comparison on the back of the wheels
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(a) Instantaneous and (b) time averaged velocity magnitude, DES
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(a) Instantaneous and (b) time averaged velocity magnitude, URANS
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Instantaneous vorticity magnitude: (a) DES, (b) URANS
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Time averaged DES cut: (a) total kinetic energy, (b) resolved Reynolds stress, (c) modeled Reynolds stress, (d) total Reynolds stress
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Time averaged URANS cut: (a) total kinetic energy, (b) resolved Reynolds stress, (c) modeled Reynolds stress, (d) total Reynolds stress
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Total landing gear force power spectrum

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