airfoil geometry in gambit
 

can anyone please help to create an airfoil( say thickness =2 m) in the gambit. please also suggest the computational boundaries of the airfoil too, please help me out i shall be very very grateful.

This may help you:

https://confluence.cornell.edu/displ...irfoil-+Step+1

https://confluence.cornell.edu/displ...arning+Modules

(i think that you mean chord length = 2m)

For the profile coordinates, you can use this:

http://www.mh-aerotools.de/airfoils/javafoil.htm