Mechanical Engineering Faculty Research
Title
Application of a Nonlinear Computational Aeroacoustics Code to the Gust-Airfoil Problem
Document Type
Article
Publication Date
Winter 2-2006
Abstract
A time-domain solution of the gust-airfoil problem is obtained using a high-accuracy computational aeroacoustics code to solve the nonlinear Euler equations. For computational efficiency, the equations are cast in chain-rule curvilinear form, and a structured multiblock solver is used on a distributed-memory parallel computer cluster.
Publication Title
AIAA Journal
Volume
44
Issue
2
First Page
323
Last Page
328
Recommended Citation
Hixon, R.; Golubev, V.; Mankbadi, R. R.; Scott, J. R.; Sawyer, Scott; and Nallasamy, M., "Application of a Nonlinear Computational Aeroacoustics Code to the Gust-Airfoil Problem" (2006). Mechanical Engineering Faculty Research. 832.
https://ideaexchange.uakron.edu/mechanical_ideas/832