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The high-order schemes
embedded in AEROFLO are coupled with an efficient
multi-grid overset capability and result in relatively
easy means to simulate complex aircraft geometries.
Sample results for a Boeing 747 geometry (Euler and
Navier-Stokes simulations) are shown below.
Inviscid Grid |
Viscous Grid |
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Click on the pictures to download high
resolution videos |
Sample Mach number and
pressure contours |
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Click to return to AEROFLO
home page.
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