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A NACA 0012 Airfoil is placed in a wind tunnel with the following free stream conditions:
Reynolds Number : 2.88e6
x velocity: 1 m/s
viscosity:
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3.4722e-7
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kg/m*s
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Using
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FLUENT,
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we
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will
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create
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a
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simulation
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of
...
this
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experiment.
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Afterwards,
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we
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will
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compare
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values
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from
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the
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simulation
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and
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data
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collected
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from
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experiment.
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Continue
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to
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