Unusually for me, I think this discussion is drifting too far into the physics of brake function, and wandering away from a discussion on the act of reducing the ground speed of an aircraft from landing speed to taxying speed.
Think about how you drive your car. Say you were driving along at the speed limit of 80 kph. That's close to the landing speed of a recreational aeroplane. Being an attentive driver, you see that a couple of hundred metres ahead, the traffic lights have changed to amber. Do you stomp on your brake pedal then and there? Nope. You take your foot off the GO pedal and let the rolling and air resistance start to slow your vehicle. As you approach the traffic lights, which are now showing red , you use your experience and decided to lightly press on the brake pedal to get a better rate of slowing. You monitor the effect of that application so that by the time your vehicle is about 30 metres from the traffic lights its speed is down to about 20 kph and so rolling and resistance forces can deal with slowing the vehicle to walking pace. Then you clean up the stopping process by a little more brake pressure application. At no time did you stomp on the brake pedal and cause the brake system to stop the rotation of the wheels completely so that they skid over the road surface.
Now, what's the difference between the braking process you have been doing since you were a pimply-faced teenager and the one you employ now as a responsible PIC?
In going to Tundra tyres, I would look at the possibility of the tyres interfering with stall characteristics, because they may increase drag, which may affect pitch behaviour. There could be prop-strike problems if the sidewalls flexed too much on touching down. That flexing could also allow the sidewalls to contact surrounding assemblies, damaging the tyre, and even the assembly.