This document provides an overview of airfoil theory as it relates to axial flow turbomachines. It discusses: 1) The assumptions of 1D flow analysis in axial turbomachines, including an infinite number of blades of negligible thickness and uniform flow. 2) How isolated airfoil theory is needed in practice due to a finite number of blades, which allows for blade-to-blade flow variations. 3) How isolated airfoil theory models each blade as a stationary airfoil in a stream of relative flow, and defines the angle of attack and lift and drag forces on the airfoil.