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April 24, 2006, 16:21
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Please explain
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#1 |
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Guest
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In tutorial 8:supersonic flow over a wing, there is an expression (Pressure+101325[Pa])*Normal X, can someone explain to me what Normal X is ?
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April 25, 2006, 06:18
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Re: Please explain
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Guest
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It's the x component of the normal vector on a surface.
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