I only have about 15 hours in Citabrias, so I'm speaking from general experience and not make/model experience. Much of the time, the real restriction on aircraft performance is the pilot, not the airplane. Adding doodads to an airplane can be a benefit, but often they add a benefit in one area but cause a detriment in others. For instance, my former hangar neighbor had VGs on his 172 and bragged about how it improved his control at "slow" approach speeds--which he did at 70 knots. My reaction was that 70 knots is not "slow" for a 172. His was a 172M model, with Cessna's slightly cuffed leading edge and curved wingtips, giving a 44 knot/50 mph stall speed; 1.3 Vso = 57 knot/65 mph--at gross weight. My 63 P172D has the stock leading edge (no cuff) but really droopy tips, which add control at slow airspeeds but don't lower the stall speed perceptibly. The book says mine should stall at 52 mph, but I routinely do my approaches at 55-60 mph when lightly loaded and 65-70 mph at gross. Your actual flying weight affects your stall speed and your approach speed considerably.
The downside to VGs has been mentioned--harder to clear off frost, snagging on fuel hoses, etc. The real downside is their cost, if you don't actually use them. Spending $1500 on something that you don't really use is pretty wasteful.
You might consider going out and see what your actual stall speed is per your airspeed indicator at the weights you normally use, and then practice at 1.3 x your indicated stall speed. Good guess that you will find that you've been using a higher than necessary approach speed, which makes a huge difference in how short your airplane can land. Similarly, Vx and Vy are affected a bunch by your airplane's actual weight as well as by density altitude. But the only way to know what your airplane is capable of doing is to find out, perhaps with instruction, perhaps with just some definitive practice.
Cary