That all seems correct but with a wing tip vortex keep in mind that it's the airspeed difference between the air flowing around the wing vs free airflow adjacent to the wing, thus the speed difference, thus the vortex, so even a chord neutral shape works and produces little to no drag.tok-tokkie wrote:When I was at University ('72 - '75) wingtip vorteces were said to be as a result of the different speed of the air over the top compared to underneath - resulting from the different camber & the angle of attack of the two sides. The diagram you link to was used. The analytical theory showed that mathematically there is circulation of the air about the wing which is shed at the tip. So what should be done here? An aerofoil with different curvature each side or a symmetrical one set slightly off straight ahead? Or do you get them from just about anything. I am aware that smokestacks shed vortexes but they come off one side then the other with opposite rotation & buffet the smokestack badly (hence the spiral rids on the outside to prevent vortex shedding).
As for your smokestack example, keep in mind that a round shape produces a large unstable, turbulent wake, whereas an airfoil does not.