PEGASUS 5 Examples
- NACA 0012 Airfoil:
A simple two-dimensional c-grid embedded in two box grids.
3 zones and 74K grid points.
- Sphere:
A simple three-dimensional spherical grid embedded in a box grid.
2 Zones and 48K grid points.
- Wing-Body:
A three-dimensional wing and fuselage.
7 zones and 2.62 million grid points.
- Business Jet:
A Generic Business Jet, including wing, fuselage, and engine.
13 zones and 3.52 million grid points.
- Internal flow example:
A duct with a sphere embedded inside.
2 zones and 106K grid points.
For each example case, you can download a gzipped .tar file which
contains the example. Each example includes a PEGASUS 5 input file,
sample output (log) files, input grid files, and an overflow input
file. The contents will look something like this:
- peg.i
- sample.mpi.log
- overflow/overflow.inp
- X_DIR/name1.x
- X_DIR/name2.x
- .....
- X_DIR/namen.x
where name* is the descriptive name of each zone, and match the
names used in the peg.i input file. The input grid files are stored
as required for input into PEGASUS 5, in individual files (one zone
per file) in the X_DIR subdirectory. The grid files are stored as
FORTRAN double-precision big-endian unformatted data files.
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