Sign-up for free online course on ANSYS simulations!Problem 1
Consider the incompressible, inviscid airfoil calculation in FLUENT presented in class. Recall that the angle of attack, α, was 5°.
...
where α is in degrees.
Go to Problem 2
Page History
Overview
Content Tools
Consider the incompressible, inviscid airfoil calculation in FLUENT presented in class. Recall that the angle of attack, α, was 5°.
...
where α is in degrees.
Go to Problem 2