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Modal element method for potential flow in non-uniform ducts: Combining closed form analysis with CFDAn analytical procedure is presented, called the modal element method, that combines numerical grid based algorithms with eigenfunction expansions developed by separation of variables. A modal element method is presented for solving potential flow in a channel with two-dimensional cylindrical like obstacles. The infinite computational region is divided into three subdomains; the bounded finite element domain, which is characterized by the cylindrical obstacle and the surrounding unbounded uniform channel entrance and exit domains. The velocity potential is represented approximately in the grid based domain by a finite element solution and is represented analytically by an eigenfunction expansion in the uniform semi-infinite entrance and exit domains. The calculated flow fields are in excellent agreement with exact analytical solutions. By eliminating the grid surrounding the obstacle, the modal element method reduces the numerical grid size, employs a more precise far field boundary condition, as well as giving theoretical insight to the interaction of the obstacle with the mean flow. Although the analysis focuses on a specific geometry, the formulation is general and can be applied to a variety of problems as seen by a comparison to companion theories in aeroacoustics and electromagnetics.
Document ID
19940011326
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Baumeister, Kenneth J.
(NASA Lewis Research Center Cleveland, OH, United States)
Baumeister, Joseph F.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1994
Subject Category
Numerical Analysis
Report/Patent Number
NAS 1.15:106347
E-8118
NASA-TM-106347
AIAA PAPER 93-0813
Report Number: NAS 1.15:106347
Report Number: E-8118
Report Number: NASA-TM-106347
Report Number: AIAA PAPER 93-0813
Meeting Information
Meeting: Aerospace Sciences Meeting and Exhibit
Location: Reno, NV
Country: United States
Start Date: January 10, 1994
End Date: January 13, 1994
Sponsors: AIAA
Accession Number
94N15799
Funding Number(s)
PROJECT: RTOP 505-62-52
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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