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The airplane body below is subjected to 600 mile miles per hour winds at 0 degrees to simulate it traveling mid flight. In an effort to study the flow over the wing-body junction, the velocity vectors and streamlines will be calculated.
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The airplane body below is subjected to 600 mile miles per hour winds at 0 degrees to simulate it traveling mid flight. In an effort to study the flow over the wing-body junction, the velocity vectors and streamlines will be calculated.
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