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Sparse matrix techniques applied to modal analysis of multi-section duct linersA simplified procedure is presented for analysis of ducts with discretely nonuniform properties. The analysis uses basis functions as the generalized coordinates. The duct eigenfunctions are approximated by finite series of these functions. The emphasis is on solution of the resulting large sparse set of linear equations. Characteristics of sparse matrix algorithms are outlined and some criteria for application are established. Analogies with structural methods are used to illustrate variations which can increase efficiency in generating values for design optimization routines. The effects of basis function selection, number of eigenfunctions and identification and ordering of equations on the sparsity and solution stability are included.
Document ID
19750041708
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Arnold, W. R.
(NASA Langley Research Center; George Washington University Hampton, Va., United States)
Date Acquired
August 8, 2013
Publication Date
March 1, 1975
Subject Category
Acoustics
Report/Patent Number
AIAA PAPER 75-514
Meeting Information
Meeting: American Institute of Aeronautics and Astronautics, Aero-Acoustics Conference
Location: Hampton, VA
Start Date: March 24, 1975
End Date: March 26, 1975
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
75A25780
Distribution Limits
Public
Copyright
Other

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