Viscous Flow and Pressure Coefficient

AI Thread Summary
A large positive dCp/dX significantly influences viscous flow in airfoil design, particularly by affecting the lift coefficient in relation to the angle of attack. While viscosity is independent of pressure, changes in pressure gradients can alter density and kinematic viscosity, impacting flow characteristics. The discussion emphasizes the importance of understanding the relationship between pressure coefficients and lift coefficients in both viscous and inviscid flow scenarios. For further insight, examining the lift coefficient versus angle of attack graph is recommended. This analysis is crucial for optimizing airfoil performance.
snido727
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Homework Statement


What effect does a large positive dCp/dX have on the real viscous flow? This is for an airfoil design project using thin airfoil theory + vortex panel method.




The Attempt at a Solution


As far as I know Viscosity is independent of pressure, so the only thing I can think of is assuming ideal gas behavior and saying that it affects the density and therefore the kinematic viscosity. However I believe that he is referring to something different, some property of a viscous flow that I haven't yet figured out.

Thanks in advance.
 
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Can anyone help me? I don't need the answer so much as a nudge in the right direction...ie "look at x property"

Thanks again
 
in which dimension is flow?
 
The design is in 2 dimensions.
 
Well for anyone else who stumbles upon this and needs the answer look at the difference between the lift coefficient vs. angle of attack graph for viscid vs. inviscid flow, and consider how the coefficient of pressure affects the lift coefficient.
 
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