Well, first off, it's because military fighters don't have "V-speeds". That's something you get in civilian aviation for standardization.
More correctly, though, is because fighters don't have a "stall speed" per se -- it is measured by AOA. In fact, the F-15E and T-38, the jets that I have the most time in, don't have a published "stall speed" anywhere in the literature. Stall is measured by AOA as well as environmental factors (like knowing when the buffett you're feeling on the airframe has reached an intensity to the point where the aircraft is actually stalled).
Why? Because the stall speeds change, depending on fuel and stores load. It's not a static number. Again, AOA is the only reliable method of actually determining when the airplane is stalled. Also, remember that for jets that are maneuvering, stall AOA can be reached at a wide range of airspeeds through the flight envelope (e.g., accelerated stalls) and that is something that can be used during tactical maneuvering.
Even at that, the AOA number doesn't dictate how slow I can actually fly in a fighter. I have flown F-15Es and T-38s well below what would be those stall speeds -- at high AOA and in afterburner. The AOA says that the airplane is fully stalled, and yet I can fly airspeed/altitude/heading to Commercial PTS standards. Same thing as when you see the Blue Angles fly the F-18 at high AOA but very slow; the airspeed is well below where the airplane would stall if it were just relying on Mr Bernoulli for lift, but the airplane is still most definitely flying controlled.
So, knowing those speeds doesn't really help anyone understand the issue.