Abstract
T Falkner-Skan type equations are established for a compressible laminar boundary layer on a rotating body in axial flow. The coupling between the axial and circumferential flows is analyzed and the effect of rotation rate upon the velocity profiles is shown. Similar solutions are used for the polynomial representation of the integral quantities. The shape factor H is computed as an example. Finally, the independence of the integral quantities on co is established, leading to a very useful universality of the polynomial representation.
Full Text 
Sign-in/Register to access full text options
Sign-in/Register to access full text options 
Published version (
Free)
Free) 
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a call
