Hi,
I am no expert on model aircraft but i do know allot about aerofoils, being a professional aerodynamicist! NACA aerofoils are a good start and you can easily get coordinates for them. You may find others at that site too.
http://www.ae.uiuc.edu/m-selig/ads/coord_database.html
You want something with high lift and low drag so you will want a laminar flow aerofoil. A model aircraft will be working at very low reynolds numbers. Symmetrical aerofoils are simple to make and have minimal drag, a NACA 0012 or 0015 might work if you incline it to the oncoming flow by 2-3degrees. Alternatively a cambered NACA aerofoil like a 63-415 might work well. Hope that helps a bit. It really depends on allot of factors such as the wing chord, taper ratio etc. If you give me a few more details i might be able to help more.