Induced Angle of Attack Calculator

Posted by Dinesh on

Use this aerodynamics calculator to calculate the induced angle of attack for your aerodynamics problems.

Calculate Induced Angle of Attack

Lift coefficient (CL) :
Aspect ratio (A):
?i :

Formula:

?i = CL / ( ? × A )

where,
CL - Lift coefficient
? - 3.142857142857143
A - Aspect ratio
?i - Induced angle of attack (rad)