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Title: |
A Navier-Stokes solution of the three-dimensional viscous compressible flow in a centrifugal compressor impeller
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Author(s): |
Harp, J. L., Jr.
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Abstract: |
A two-dimensional time-dependent computer code was utilized to calculate the three-dimensional steady flow within the impeller blading. The numerical method is an explicit time marching scheme in two spatial dimensions. Initially, an inviscid solution is generated on the hub blade-to-blade surface by the method of Katsanis and McNally (1973). Starting with the known inviscid solution, the viscous effects are calculated through iteration. The approach makes it possible to take into account principal impeller fluid-mechanical effects. It is pointed out that the second iterate provides a complete solution to the three-dimensional, compressible, Navier-Stokes equations for flow in a centrifugal impeller. The problems investigated are related to the study of a radial impeller and a backswept impeller.
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NASA Center: |
NASA (non Center Specific)
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Publication Date: |
JAN 1, 1977
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Document Source: |
Other Sources |
No Digital Version Available: |
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Document ID: |
19780028394
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Accession ID: |
78A12303
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Publication Information: |
Number of Pages = 19 |
Meeting Information: |
Transonic flow problems in turbomachinery, February 11-12, 1976, Monterey, CA |
Keywords: |
CENTRIFUGAL COMPRESSORS; COMPRESSIBLE FLOW; COMPUTER TECHNIQUES; NAVIER-STOKES EQUATION; ROTOR BLADES (TURBOMACHINERY); THREE DIMENSIONAL FLOW; VISCOUS FLOW; BOUNDARY LAYER SEPARATION; COMPUTER PROGRAMS; FINITE DIFFERENCE THEORY; FLOW VELOCITY; ITERATION; STEADY FLOW; TRANSONIC FLOW; VORTICES;
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Notes: |
In: Transonic flow problems in turbomachinery; Proceedings of the Workshop, Monterey, Calif., February 11, 12, 1976. (A78-12286 02-02) Washington, D.C., Hemisphere Publishing Corp., 1977, p. 309-323; Discussion, p. 323-327. NASA-supported research. |
Accessibility: |
Unclassified; Copyright; Unlimited; Publicly available; |
Updated/Added to NTRS: |
2004-11-03 |
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