PUMA
run on
GSS geometry
Coarse grid runs using double precision with yaw=0 deg
Ran on
ruth.cac.psu.edu
with 8 nodes (requires 573 MB memory)
Results after 4 orders reduction in norm (converged)
Second order run:
Click here for animation of convergence
M=0.065 run
Residual history
Convergence history
PUMA input file
PUMA restart file (binary)
Tecplot ASCII data (for surface only)
Tecplot ASCII data (for entire flowfield)
Contours of u-component of velocity at location B
(
PS file
,
Tecplot Layout File
,
Just lines
-
PS
)
Coarse grid runs using double precision with yaw=30 deg
Ran on
ruth.cac.psu.edu
with 8 nodes (requires 573 MB memory)
Results after 3 orders reduction in norm (converged)
Second order run:
M=0.30 run
Residual history
Convergence history
PUMA input file
PUMA restart file (binary)
Tecplot ASCII data (for surface only)
Tecplot ASCII data (for entire flowfield)
Plot of pressure
Plot of C_p
Bigger plot of vector of U-U_inf
Comparison with experiments:
Flight deck
Front part of Bridge deck
Middle part of Bridge deck
Tecplot 7.0 layout file for the above data files:
template.lay
. Edit the layout file to replace PUT_PLT_FILENAME_HERE in the 2nd line with the actual ".plt" file name
Note: All plots are plots of
U/Uinf
where
U
is the total velocity and
Uinf
is the freestream velocity (
20.83
m/s). The tecplot data files contain only the ship surface data, and not the data on the entire domain of computation
©
Anirudh Modi