Index of /~zjw/hiocfd/naca0012
Name Last modified Size Description
Parent Directory 08-May-2012 11:51 -
naca0012_level1.m2w.msh 20-May-2011 03:55 8.8M
naca0012_level1.msh 20-May-2011 04:10 8.6M
naca0012_level2.m2w.msh 20-May-2011 03:55 2.2M
naca0012_level2.msh 20-May-2011 04:10 2.1M
naca0012_level3.m2w.msh 20-May-2011 03:55 548k
naca0012_level3.msh 20-May-2011 04:10 517k
naca0012_level4.m2w.msh 20-May-2011 03:55 145k
naca0012_level4.msh 20-May-2011 04:10 129k
naca0012_level5.m2w.msh 20-May-2011 03:55 40k
naca0012_level5.msh 20-May-2011 04:10 33k
naca0012_level6.m2w.msh 20-May-2011 03:55 13k
naca0012_level6.msh 20-May-2011 04:10 9k
Grids for the C1.3 and C3.4 test cases (Naca0012 with modified X4 coefficient)
at subsonic inviscid, transonic inviscid and subsonic viscous flow conditions:
subsonic inviscid flow conditions:
M = 0.5
alpha = 2.0 (deg)
transonic inviscid flow conditions:
M = 0.8
alpha = 1.25 (deg)
subsonic viscous flow conditions:
M = 0.5
alpha = 1 (deg)
Re = 5000
linear grids
naca0012_level1.msh 114,688 cells
naca0012_level2.msh 28,672 cells
naca0012_level3.msh 7,168 cells
naca0012_level4.msh 1,792 cells
naca0012_level5.msh 448 cells
naca0012_level6.msh 112 cells
Note, that these grids have been generated by DLR in the ADIGMA project
(version 1.3 of the grids for the MTC1 & MTC2 & MTC4 test cases). The grids
have further been modified by moving the wall boundary points to match the
NACA geometry definition including the modified x^4 coefficient used in the
workshop.
quadratic grids (lines at wall boundary are given by polynomials of degree 2)
naca0012_level1.m2w.msh 114,688 cells
naca0012_level2.m2w.msh 28,672 cells
naca0012_level3.m2w.msh 7,168 cells
naca0012_level4.m2w.msh 1,792 cells
naca0012_level5.m2w.msh 448 cells
naca0012_level6.m2w.msh 112 cells
These grids have been generated by DLR based on the naca0012_level*.msh grids.
Note, that the precision of wall boundary points of the current version of
grids is increased in comparison to the version (2/24/11) of the grids.