Not getting shell meshing
 

I am trying to reproduce the wing - body tutorial given in ANSYS ICEM CFD 14 training material. Every things else is fine including density box, volume meshing and smoothing. But I am not able to get the the shell meshing as given in the included file. At leading edge autoblock is used as instructed in tutorial.

My mesh seems like this :
http://img651.imageshack.us/img651/3585/shell1p.png
http://img16.imageshack.us/img16/8655/shell2w.png

Far you have great experience in Structured meshing and you are facing problem in simple unstructured meshing, feels odd :o
well i exactly dont know the solution but once i came across this problem for another geometry but when i changed my file import from acis to parasolid or vice-versa(as i dont remember exactly), the problem gets solved but it was just a good luck :)

Actually this was done to record the youtube tutorials, and finally I solved the problem. Now this problem is solved. http://www.cfd-online.com/Forums/ans...tra-prism.html


Rigth now I am working on the youtube clip regarding NACA 0015 wing with hexa meshing.