Abstract
For constant pressure boundary layers, a simple relationship between the laminar and turbulent skin-frictions has been suggested. At a given Reynolds number, the turbulent skin-friction is found to be ~ (laminar skin-friction)0.3.
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
