@PapaKernels I see some other people have answered your question. But most people don’t understand the uses for each kind of wing. But ChiChiWerx did make a post about the wings a few years back. I can’t find it now, and his explanation was complicated, so:
Flat bottom creates the most lift and the most induced drag. This kind of airfoil has forgiving stall characteristics as well. Use this when low drag is not a priority, i.e. GA aircraft.
Symmetric creates the least lift and even requires positive AoA to do so. It does have the least induced drag at 0* AoA (duh, I mean, induced drag only exists when lift is created). Its stall characteristics also have totally, absolutely nothing to be desired. Induced drag can get high when the AoA is high (i.e. when a lot of lift is needed). This may be a bad thing, but some planes (like the Concorde) use it to their advantage as an alternative to spoilers. This type of airfoil is used almost exclusively for the supersonic bois, for which high lift and a high critical AoA is not desired, but low drag is the utmost priority.
Semi-symmetric takes the middle ground. It still creates a decent amount of lift at 0 AoA but still has less drag than the FB airfoil. Obviously, this type of wing is used for subsonic jets, which still fly fast (so they care about drag) but can still afford to (and sometimes need to) create some more lift.
By the way, I have flown the C172 a few times irl, and fly A320s a lot in flight simulators at home. The two planes use the FB and SS type airfoils respectively. Believe me, there is a big difference, although for the most part it is not experienced in SP. There are subtle differences that most do not notice.

Oh one more thing I have started the primarily sketch for a professional profile pic. I would put in a picture but because I have horrible internet I cant upload it to the site I use so you just have to take my word on it for now. I've been trying for about 20 minutes now.