The world’s Largest Sharp Brain Virtual Experts Marketplace Just a click Away
Levels Tought:
Elementary,Middle School,High School,College,University,PHD
| Teaching Since: | May 2017 |
| Last Sign in: | 408 Weeks Ago, 4 Days Ago |
| Questions Answered: | 66690 |
| Tutorials Posted: | 66688 |
MCS,PHD
Argosy University/ Phoniex University/
Nov-2005 - Oct-2011
Professor
Phoniex University
Oct-2001 - Nov-2016
The axis of a long circular cylinder is perpendicular to the undisturbed velocity of an unconfined air stream. For an inviscid fluid the velocity adjacent to the surface of the cylinder would be 2U sin θ , where U denotes the velocity far upstream and θ the angle between the radius and the initial flow direction. Neglecting changes of elevation and assuming that the pressure in the wake is sensibly uniform and that there are no discontinuities of pressure anywhere, estimate the position at which the boundary layer separates if the measured drag coefficient is 1.24. Why will this estimate be somewhat in error?
Â
Hel-----------lo -----------Sir-----------/Ma-----------dam-----------Tha-----------nk -----------You----------- fo-----------r u-----------sin-----------g o-----------ur -----------web-----------sit-----------e a-----------nd -----------acq-----------uis-----------iti-----------on -----------of -----------my -----------pos-----------ted----------- so-----------lut-----------ion-----------.Pl-----------eas-----------e p-----------ing----------- me----------- on-----------cha-----------t I----------- am----------- on-----------lin-----------e o-----------r i-----------nbo-----------x m-----------e a----------- me-----------ssa-----------ge -----------I w-----------ill----------- be-----------