Mechanical Engineering Faculty Research
Title
Comparison of Numerical Schemes for a Realistic Computational Aeroacoustics Benchmark Problem
Document Type
Article
Publication Date
Fall 10-2004
Abstract
In this work, a nonlinear block-structured CAA solver, the NASA Glenn Research Center BASS code, is tested on a realistic CAA benchmark problem in order to ascertain what effect the high-accuracy solution methods used in CAA have on a realistic test problem.
Publication Title
Aeroacoustics
Volume
3
Issue
4
First Page
379
Last Page
397
Recommended Citation
Hixon, R.; Nallasamy, M.; Sawyer, Scott; and Dyson, R., "Comparison of Numerical Schemes for a Realistic Computational Aeroacoustics Benchmark Problem" (2004). Mechanical Engineering Faculty Research. 851.
https://ideaexchange.uakron.edu/mechanical_ideas/851
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