Search Results

Showing results 1 to 2 of 2
Search took 0.00 seconds. Search: Posts Made By: Santos-Dumont

Forum: FLUENT

May 9, 2011, 11:49

Replies: 14

Getting lift force at zero angle of attack

Views: 5,927

Posted By Santos-Dumont

Correction, NACA 0012 gets 0 lift at 0°. But if...

Correction, NACA 0012 gets 0 lift at 0°.
But if the Cl your calculate is at an order as low as 10^-6, you can consider it as zero.

Forum: FLUENT

May 9, 2011, 11:38

Replies: 14

Getting lift force at zero angle of attack

Views: 5,927

Posted By Santos-Dumont

Hi, It's normal, most of the airfoils get a...

Hi,

It's normal, most of the airfoils get a zero lift at around -2°. Check your profile's polar to find out (look for the "Theory of Wing sections" .pdf on the Internet).

Showing results 1 to 2 of 2

Forum Jump

All times are GMT -4. The time now is 23:49.