Viscous flow analysis using a parallel unstructured multigrid solver

AIAA Journal ◽  
2000 ◽  
Vol 38 ◽  
pp. 2067-2076
Author(s):  
Dimitri J. Mavriplis
Keyword(s):  
Viscous Flow ◽  
Flow Analysis ◽  
Multigrid Solver

Viscous Flow Analysis Using a Parallel Unstructured Multigrid Solver

AIAA Journal ◽  
10.2514/2.894 ◽  
2000 ◽  
Vol 38 (11) ◽  
pp. 2067-2076 ◽  
Author(s):  
Dimitri J. Mavriplis
Keyword(s):  
Viscous Flow ◽  
Flow Analysis ◽  
Multigrid Solver

Cascade viscous flow analysis using the Navier-Stokes equations

1987 ◽  
Vol 3 (5) ◽  
pp. 406-414 ◽  
Author(s):  
Roger L. Davis ◽  
Ron-Ho Ni ◽  
James E. Carter
Keyword(s):  
Viscous Flow ◽  
Stokes Equations ◽  
Flow Analysis ◽  
Navier Stokes ◽  
Navier Stokes Equations

3D viscous flow analysis on wing-body-aileron-spoiler configurations

2005 ◽  
Vol 9 (6) ◽  
pp. 476-484 ◽  
Author(s):  
Ralf Mertins ◽  
Eberhard Elsholz ◽  
Samira Barakat ◽  
Birol Colak
Keyword(s):  
Viscous Flow ◽  
Flow Analysis

Viscous flow analysis of advanced particle separators

1992 ◽  
Vol 8 (4) ◽  
pp. 843-848 ◽  
Author(s):  
M. Zedan ◽  
A. Mostafa ◽  
P. Hartman ◽  
A. Sehra
Keyword(s):  
Viscous Flow ◽  
Flow Analysis

Three-Dimensional Flow Phenomena in a Transonic, High-Through-Flow, Axial-Flow Compressor Stage

1992 ◽  
Author(s):  
William W. Copenhaver ◽  
Chunill Hah ◽  
Steven L. Puterbaugh
Keyword(s):  
Flow Field ◽  
Viscous Flow ◽  
Numerical Technique ◽  
Flow Analysis ◽  
Three Dimensional ◽  
Axial Flow ◽  
Compressor Stage ◽  
Complex Flow ◽  
Pressure Transducers ◽  
Through Flow

A detailed aerodynamic study of a transonic, high-through-flow, single stage compressor is presented. The compressor stage was comprised of a low-aspect-ratio rotor combined alternately with two different stator designs. Both experimental and numerical studies are conducted to understand the details of the complex flow field present in this stage. Aerodynamic measurements using high-frequency, Kulite pressure transducers and conventional probes are compared with results from a three-dimensional viscous flow analysis. A steady multiple blade row approach is used in the numerical technique to examine the detailed flow structure inside the rotor and the stator passages. The comparisons indicate that many flow field features are correctly captured by viscous flow analysis, and therefore unmeasured phenomena can be studied with some level of confidence.

scholarly journals Three-Dimensional Viscous Flow Analysis of Compressor Cascade Channels.

1993 ◽  
Vol 59 (561) ◽  
pp. 1524-1531
Author(s):  
Hidenori Yoshida ◽  
Takashi Kawashima ◽  
Keiji Sakagawa
Keyword(s):  
Viscous Flow ◽  
Flow Analysis ◽  
Three Dimensional ◽  
Compressor Cascade
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