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Transonic cascade flow calculations using non-periodic C-type gridsA new kind of C-type grid is proposed for turbomachinery flow calculations. This grid is nonperiodic on the wake and results in minimum skewness for cascades with high turning and large camber. Euler and Reynolds averaged Navier-Stokes equations are discretized on this type of grid using a finite volume approach. The Baldwin-Lomax eddy-viscosity model is used for turbulence closure. Jameson's explicit Runge-Kutta scheme is adopted for the integration in time, and computational efficiency is achieved through accelerating strategies such as multigriding and residual smoothing. A detailed numerical study was performed for a turbine rotor and for a vane. A grid dependence analysis is presented and the effect of artificial dissipation is also investigated. Comparison of calculations with experiments clearly demonstrates the advantage of the proposed grid.
Document ID
19910011758
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Arnone, Andrea
(NASA Lewis Research Center Cleveland, OH, United States)
Liou, Meng-Sing
(NASA Lewis Research Center Cleveland, OH, United States)
Povinelli, Louis A.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1991
Publication Information
Publication: Computational Fluid Dynamics Symposium on Aeropropulsion
Subject Category
Fluid Mechanics And Heat Transfer
Accession Number
91N21071
Funding Number(s)
CONTRACT_GRANT: NASA ORDER C-99066-G
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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