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Panel - Compressible Flow over a Wing-Body Junction
Panel - Compressible Flow over a Wing-Body Junction(Tutorial Name) - Panel(Tutorial Name) - Panel

Problem Specification

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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