During launcher ascent, dynamic pressure evolution is describe in
this answer for the Saturn V.
I suppose this is comparable from one launcher to another.
Given the protections designed for reentry, I suppose dynamic pressure involved during reentry are more important than during ascent.
What does this evolution looks like for reentry?
Do it looks like the same (bell shape increase and decrease with almost the same shape)? If the answer is quite different from one spaceship to another,
this question can be narrowed to Apollo or other manned ships.