I am a bit struggling to understand the exact meaning of the pitching moment (and coefficient) regarding liftoff. As I understand, at 0° of angle of attack, we want negative pitching moment coefficient (I will call it Cm) to have what is considered a "stable car". It is usually observed to be just below 0 from the sources I have seen. However, when the car is pitched about its rear axle, the Cm grows.
When Cm is above 0 it means that upon a disturbance at the front, the car will pitch more and more. However, the aero loads have to be counted as well. My question is:
I have a car with let's say a Cm that crosses 0 at 4° of elevation angle (again, about the rear axle). In order to have 0N on the front axle (which means having to lift half the car's weight if the weight distribution is 50/50), we need to first overcome the aero load, and then the car weight. I have seen that this happens at about 18°.
What should I understand with this? I am a bit confused. I don't see how passed 4° the car would pitch more and more without overcoming the front axle load since the wheels are already in the air. I think I am missing something (elementary) there but cannot figure out what.