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AEROFLO Sample Problems (Desktop Version Only)
These
problems involve both canonical and more complicated
problems with complex geometries and/or flow physics. The
complex problems usually require the use of multiple
computational grid blocks, for which AEROFLO must be
executed in parallel. Instructions on AEROFLO execution
in parallel are contained in the problem description.
Note
the emphasis, for the more geometrically complex
problems, is on the high-order accurate methods that are used
for these problems, in spite of the complexity in the
geometries of the problems.
The
following is a list of the problems. Click on each link
to access problem description, set up files, and the
computational grids used for the calculations. Comparison
of AEROFLO results with experimental data and/or other
numerical results are also provided.
Converging-Diverging
Nozzle
Shu-Osher Shock Tube Problem
Hypersonic
Flow past a Cylinder
Flow
past a Cylinder
Flow
past a Cylinder (Multiblock)
Shock-Boundary
Layer Interaction
Laminar
flow over a Flat Plate
Laminar
flow over a Flat Plate (Multiblock)
Turbulent
flow over a Flat Plate
Flow
over an Airfoil (NACA0012)
Flow
over an Airfoil (NACA0012) (Multiblock)
Flow over an Airfoil
(RAE2822)
Backward-Facing
Step
Flow
past a wedge
Prandtl-Meyer
Expansion over a 15o corner at Mach
=2.5
Onera M6 Wing Calculations
Onera M6 Wing Calculations (Multiblock)
Boeing
747 Airplane
HIFiRE Flight Test Article
Flow Past a V-Gutter Bluff
Body
Acoustic Characteristics of a
3D Jet
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