Javafoil online dating

It fails to converge with small irregularities, and crashes kind of a lot.

Java Foil never complains, but results are optimistic (Inviscid analysis = more lift and less drag).

Lucky for me, I landed right near the optimum flap angle from the get go, so optimizing was pretty easy.

I did 5 flap iterations, maximizing the slot for eash setup.

Its pretty extreme foil tho- the tail is seperated at all AOA's, and the high pressure side seperates below 6*.Definately worth browsing before delving any deaper.Helped with a lot of the basic theory about lift, thin airfoil theory, max lift theory, etc.I'll have to do more digging about the accuracy of multi-elements in Java work Josh, that's interesting stuff, well done on documenting it, I find that always helps it sink in properly for me Thanks for the link to that e-textbook, that'll be an interesting read, I always find it jogs my memory and a few new points are raised even when going over stuff already learnt, and of course any new material is even better!i've learned a few things while researching blunt trailing edges (google flatback airfoils for more info). whats relevant to this section is that a blunt trailing edge airfoil can be modeled with an open end, instead of trying to create a round edge.