Direct Numerical Aeroacoustics for low Mach numbers using one Unstructured Grid
نویسندگان
چکیده
منابع مشابه
Direct Numerical Aeroacoustics for Low Mach Numbers Using One Unstructured Grid
Using an unstructured grid, for which the mesh size is adapted to the local flow and acoustic solution, one can reduce the number of unknowns needed for a direct aeroacoustic simulation. The compressible Navier-Stokes equations for Mach numbers 0 < M < 1 are considered. However, the unstructured grid together with the increasing stiffness of the problem for M → 0 reveals new numerical challenge...
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ژورنال
عنوان ژورنال: ESAIM: Proceedings
سال: 2007
ISSN: 1270-900X
DOI: 10.1051/proc:2007007