1) Static pressure is the result of constraining a fluid, meaning a collection of particles, in a finite space. This will force the particles on a microscopic level to interact either in (elastic) collisions (such as in a dilute gas) or in more complex interactions of repulsive and attractive forces. The result of the presence of other particles is felt on a macroscopic level as a force per area (the particles push each other away), pressure.
2) Fluid statics is a model that artificially freezes the state of a liquid. In reality even macroscopic equilibrium never means uniformity but instead always allows for a certain amount of variance (Just think of the Brownian motion of particles in seemingly static fluids!), generally characterised by a certain Gaussian distributions. A fluid is simply a collection of particles that interact. Even in thermal equilibrium not all particles have the same energy content, the same kinetic energy, but they are stochastically distributed around a certain mean value. While at continuum level this fundamental property of restlessness is neglected and lumped into macroscopic properties such as pressure, viscosity or the equation of state, the fact the a fluid is never truly at rest, is the reason for any macroscopic property. As already pointed out the static pressure of flowing fluids is caused by molecular motion. In a moving fluid this motion is though - contrarily to a resting fluid - partially directed by the macroscopic flow velocity. As a result collisions will dominate in the flow direction while be significantly lower perpendicular to it. This results in a different perception of pressure (a certain anisotopy). The anisotropic part of pressure that is caused by the macroscopic flow with velocity $\vec u$ is termed dynamic pressure $p_d = \sum\limits_i \frac{\rho u_i u_i}{2}$ while the part that is isotropic (in all directions identical) is called the static pressure $p$ (It is also perceived by a element perpendicular to the flow direction). The combination of the two is felt at a stagnation point if the flow is slowed down isentropically: The stagnation pressure $p_s$ is the sum of the former two.
3) Such a completely uniform flow is impossible in a real world as any sort of friction introduces a flow profile that is zero towards the walls (no-slip boundary). This friction results in a loss of energy and thus a pressure gradient, a pressure drop. Theoretically one can look at flow as you describe it with an inviscid flow model (there is no friction, Euler equation, this model does not have to respect the no-slip boundary condition). The Bernoulli equation for such a flow would be
$$ p_1 + \rho \frac{u_1^2}{2} + \rho g h_1 = p_2 + \rho \frac{u_2^2}{2} + \rho g h_2 $$
For a velocity that stays the same between point 1 and 2 which also is at the same level $h_1 = h_2$ the static pressure has to take the same non-zero value. Its precise value can be determined by the equation of state, such as the ideal gas law
$$ p v = R_m T. $$
4) I have just given an answer to your fourth question on another post of yours. In short: Any pressure gradient can be interpreted by either reducing the mean free path (for a compressible ideal gas) or pressing the building bricks of an incompressible fluid (e.g. molecules) closer together exerting a increasing force and thus a larger pressure onto each other.