An Overset Finite-Element Large-Eddy Simulation Method With Applications to Turbomachinery and Aeroacoustics
Author:
Affiliation:
1. Institute of Industrial Science, University of Tokyo, Tokyo, Japan
2. Mechanical Engineering Research Laboratory, Hitachi Ltd., Ibaraki, Japan
3. Research & Development Laboratory, Hitachi Industries Co., Ltd., Ibaraki, Japan
Abstract
Publisher
ASME International
Subject
Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics
Link
http://asmedigitalcollection.asme.org/appliedmechanics/article-pdf/70/1/32/5469865/32_1.pdf
Reference42 articles.
1. Moore, J., Moore, J. G., and Timmis, P. H., 1984, “Performance Evaluation of Centrifugal Compressor Impellers Using Three-Dimensional Viscous Flow Calculations,” ASME J. Eng. Gas Turbines Power, 106, pp. 475–481.
2. Dawes, W. N., 1988, “Development of a 3D Navier-Stokes Solver for Application to All Types of Turbomachinery,” ASME Paper No. 88-GT-70.
3. Hah, C., Bryans, A. C., Moussa, Z., and Tomsho, M. E., 1988, “Application of Viscous Flow Computations for the Aerodynamic Performance of a Back-Swept Impeller at Various Operating Conditions,” ASME J. Turbomach., 110, pp. 303–311.
4. Denton, J. D. , 1992, “The Calculation of Three-Dimensional Viscous Flow Through Multistage Turbomachinery,” ASME J. Turbomach., 114, pp. 18–26.
5. Goto, A. , 1992, “Study of Internal Flows in a Mixed-Flow Pump Impeller at Various Tip Clearances Using Three-Dimensional Viscous Flow Computations,” ASME J. Turbomach., 114, pp. 373–382.
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