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Here's the data from the Engineering Toolbox. The
viscosity changes a factor of 4 from 80 to 200 F. That site has an
enormous amount of good information.
Does this change in
viscosity actually translate into an equal change in flow rate? If so, you
have to wonder if anyone has tested the EWP's at normal engine temps.
I know Todd had his set
up for in-flight flow measurements. How about it Todd? Did you see
significantly more flow when hot?
Rusty (Slingshot
regaining the lead for single rotor test mule)
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