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Temperature bc updated in text
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_tutorials/incompressible_flow/Inc_Laminar_Flat_Plate.md

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@@ -91,7 +91,7 @@ We also now set the temperature as part of the input to the inlet boundary condi
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MARKER_INLET= ( inlet, 297.62, 69.1687, 1.0, 0.0, 0.0 )
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```
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Defining a no-slip boundary condition for viscous walls can be accomplished in the same manner as in the compressible solver with the `MARKER_HEATFLUX` and `MARKER_ISOTHERMAL` options. The constant temperature boundary condition of 197.62 K is set on the flat plate as follows:
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Defining a no-slip boundary condition for viscous walls can be accomplished in the same manner as in the compressible solver with the `MARKER_HEATFLUX` and `MARKER_ISOTHERMAL` options. The constant temperature boundary condition of 148.81 K is set on the flat plate as follows:
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```
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% -------------------- BOUNDARY CONDITION DEFINITION --------------------------%

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