PUMA
run on
Ship geometry
Inviscid grid runs using double precision with yaw=0 deg
Ran on
grimm.aero.psu.edu
with 8 nodes (requires 1090 MB memory)
Results after 1.5 orders reduction in norm
M=0.20 run
Residual history
Convergence history
PUMA input file
PUMA restart file (binary)
Tecplot ASCII data (surface only)
Tecplot ASCII data (entire flowfield)
Plots:
U/Uinf Contours with Mesh
(
PS file
)
U/Uinf Contours without Mesh
(
PS file
)
Pressure Contours with Mesh
(
PS file
)
Pressure Contours without Mesh
(
PS file
)
Mach Contours at section Y=30
Mach Contours at section Y=0 i.e. center
Inviscid grid runs using double precision with yaw=30 deg
Click for animated gif of convergence
Ran on
grimm.aero.psu.edu
with 8 nodes (requires 1090 MB memory)
Results after 1.5 orders reduction in norm
M=0.20 run
Residual history
Convergence history
PUMA input file
PUMA restart file (binary)
Tecplot ASCII data (surface only)
Tecplot ASCII data (entire flowfield)
Plots:
U/Uinf Contours with Mesh
(
PS file
)
U/Uinf Contours without Mesh
(
PS file
)
Pressure Contours with Mesh
(
PS file
)
Pressure Contours without Mesh
(
PS file
)
Mach Contours at section Y=30
Mach Contours at section Y=0 i.e. center
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
