It was very interesting to read this post and inspired me to brush up on my boundary layer and aero theory.
Reynolds number has no effect on the laminar separation point. Increasing Reynolds number can cause a transition to turbulent boundary layer ahead of separation and effectively move...
FPα in this formula signifies the propeller or inlet force. I know this is an old thread but for anyone looking for some clarification check out the image I attached it goes over the basics from the text Aircraft Design a Conceptual Approach by Raymer