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Category 5 problem solution using an unstructured finite volume algorithmFor the simulation of flows with complex geometries, unstructured finite volume methods have proven to be very popular, and simulations of a large number of flows have been done with good results using this approach. Since most of the simulations to date were done for steady flows, it is not clear that present unstructured finite volume algorithms can accurately track the unsteady propagation of acoustic waves in a computation. Therefore, there is a need to assess the accuracy of these methods for acoustic calculations. In this paper, we perform the numerical simulation of a very small amplitude acoustic wave incident on the non-uniform steady flow in a quasi- 1 D convergent-divergent nozzle using an unstructured finite volume algorithm with piece-wise linear, least square reconstruction, Roe flux difference splitting, and second-order MacCormack time marching. First, the spatial accuracy of the algorithm is evaluated for the steady flow by running the simulation with a sequence of successively finer meshes. Then the unsteady numerical solution with the acoustic perturbation is presented.
Document ID
19950023736
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bui, Trong T.
(NASA Lewis Research Center Cleveland, OH, United States)
Mankbadi, Reda R.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1995
Publication Information
Publication: NASA. Langley Research Center, ICASE(LaRC Workshop on Benchmark Problems in Computational Aeroacoustics (CAA) p 267-272 (SEE N95-30133 10-71)
Subject Category
Computer Programming And Software
Accession Number
95N30157
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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