United States National Aeronautics and Space Administration
United States National Aeronautics and Space Administration: Publications
Accessibility Remediation
If you are unable to use this item in its current form due to accessibility barriers, you may request remediation through our remediation request form.
Document Type
Article
Date of this Version
2001
Citation
5th International Conference on Spectral and High Order Methods, Uppsala, 2001
Abstract
A method of minimizing numerical errors, and improving nonlinear stability and accuracy associated with low Mach number computational aeroacoustics (CAA) is proposed. The method consists of two levels.
Comments
Used by permission.