Article
Comparison of Numerical Schemes for a Realistic Computational Aeroacoustics Benchmark Problem
Aeroacoustics
Document Type
Article
Publication Date
10-1-2004
Disciplines
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.
Citation Information
R. Hixon, M. Nallasamy, Scott Sawyer and R. Dyson. "Comparison of Numerical Schemes for a Realistic Computational Aeroacoustics Benchmark Problem" Aeroacoustics Vol. 3 Iss. 4 (2004) p. 379 - 397 Available at: http://works.bepress.com/scott_sawyer/8/