Discuss the below:
Q: The steady plane flow in the figure has the polar velocity components vθ = Ωr and vr = 0. Determine the circulation Γ around the path shown. The response must be typed, single spaced, must be in times new roman font (size 12) and must follow the APA format
![770_Steady plane.jpg](https://secure.tutorsglobe.com/CMSImages/770_Steady plane.jpg)