"Application of a Nonlinear Computational Aeroacoustics Code to the Gust-Airfoil Problem" by R. Hixon

Selected Works of Dr. Scott Sawyer

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Application of a Nonlinear Computational Aeroacoustics Code to the Gust-Airfoil Problem

AIAA Journal

R. Hixon
V. Golubev
R. R. Mankbadi
J. R. Scott
Scott Sawyer, The University of Akron, Main Campus
M. Nallasamy

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Document Type

Article

Publication Date

2-1-2006

Disciplines

Engineering and
Mechanical Engineering

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.

Citation Information

R. Hixon, V. Golubev, R. R. Mankbadi, J. R. Scott, et al.. "Application of a Nonlinear Computational Aeroacoustics Code to the Gust-Airfoil Problem" AIAA Journal Vol. 44 Iss. 2 (2006) p. 323 - 328
Available at: http://works.bepress.com/scott_sawyer/12/