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New Member
Asif Ali
Join Date: Sep 2015
Location: Karachi
Posts: 4
Rep Power: 12 ![]() |
Dear All
I am using ansys fluent, perform analysis of 2D airfoil at low Reynolds number. Model K-epsilon, Pressure based solver. i also reduces the under relaxation factor. i am facing problem 01. continuity equation is not converges. 02. Velocity in Domain is higher than the inlet velocity. Kindly replay me here or email. asif.laghari43@gmail.com |
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