maline said:
If the whole cylinder, as a velocity field, is rigid then so is anybody contained in and moving with it.
I'm not 100% sure this addresses the derivative issue I brought up, but since I have no way of addressing that issue if it actually is an issue I'm going to assume that your statement is correct in what follows.
I'm going to take another crack at the angular momentum tensor, but this time in Cartesian coordinates, ##t, z, x, y##. I'm not entirely sure my previous computation in cylindrical coordinates was correct, because I'm not entirely sure I took proper account of the effects of curvilinear coordinates. Rather than try to fix that, I'm going to just use coordinates where we know there are no such issues.
The angular momentum tensor, as I posted before, is given by ##M^{ab} = X^a P^b - X^b P^a##, where ##X^a## is the 4-position vector and ##P^a## is the 4-momentum vector. I'm going to start by assuming constant mass density, which means we can factor out the mass density and use the 4-velocity field ##U^a## instead of the 4-momentum ##P^a##.
The general approach I am going to try is to first evaluate the 4-momentum tensor at a particular event, and then integrate over the appropriate range of spatial coordinates in the ##t = 0## plane to evaluate the total angular momentum of the object at the instant ##t = 0##. I'll start by doing this in the rest frame of the center of mass (i.e., the frame in which the motion is a "pure" rotation, no translation).
First we will evaluate the full cylinder. Here we have ##X^a = \left( t, z, R \cos ( \omega t + \phi ), R \sin ( \omega t + \phi ) \right)##, where ##R## is the (constant) radius of the cylinder, ##\omega## is the (constant) angular velocity, and ##\phi## labels each worldline by its "angular position" in the cylinder at time ##t = 0##, and so ranges from ##0## to ##2 \pi## since we are considering the full cylinder. We then have ##U^a = \left( \gamma, 0, - \gamma \omega R \sin ( \omega t + \phi ), \gamma \omega R \cos ( \omega t + \phi ) \right)##, where ##\gamma = 1 / \sqrt{1 - \omega^2 R^2}##.
The six independent components of ##M^{ab}## are then:
$$
M^{01} = - z \gamma
$$
$$
M^{02} = - \gamma R \left[ \cos ( \omega t + \phi ) + \omega t \sin ( \omega t + \phi ) \right]
$$
$$
M^{03} = - \gamma R \left[ \sin ( \omega t + \phi ) - \omega t \cos ( \omega t + \phi ) \right]
$$
$$
M^{12} = - z \gamma \omega R \sin ( \omega t + \phi )
$$
$$
M^{13} = z \gamma \omega R \cos ( \omega t + \phi )
$$
$$
M^{23} = \gamma \omega R^2
$$
The above components are at a particular event, labeled by its ##X^a## coordinates as given above. To evaluate the total angular momentum of the cylinder as a whole, at time ##t = 0##, we first set ##t = 0## in the above, and then integrate over the spatial coordinates occupied by the cylinder at ##t = 0##. The latter is a double integral:
$$
M_{\text{total}}^{ab} = \int_{-Z/2}^{Z/2} dz \int_0^{2 \pi} d\phi M^{ab} ( z, \phi )
$$
where we view each component of ##M## as a function of two variables, ##z## and ##\phi##. Note carefully the limits of integration for ##z##: we assume that the spatial origin, at ##z = 0##, is the geometric center of the cylinder, and that its total length is ##Z##, so we integrate over ##z## from ##- Z / 2## to ##Z / 2##. It should be evident that, since the trig functions integrate to zero over the range of ##\phi##, and since the function ##z## itself integrates to zero from ##- Z / 2## to ##Z / 2##, the only component which ends up nonzero after integration is
$$
M_{\text{total}}^{23} = \gamma \omega R^2 Z
$$
This means that the total angular momentum of the cylinder at ##t = 0## lies purely in the x-y plane, which is what we expect. And in fact, the same will be true at
every value of ##t##, since plugging in any constant value of ##t## in the above does not change the evaluation of any of the integrals (it adds some trig function terms but they still integrate to zero).
Now for the case of the helix. Here the only difference from the above is that ##\phi##, instead of being an independent variable labeling worldlines, is equal to ##k z##, where ##k## is the "spatial turn frequency" of the helix (this is related to the pitch, but I'm not sure if it's identical, and that detail doesn't affect what follows). Since we have that the helix does one full turn in length ##Z##, we have that ##k = 2 \pi / Z##, so ##\phi = 2 \pi z / Z##. So now, to find the total angular momentum of the helix, we have only a single integral, over ##z##, but the function of ##z## we are integrating over is more complicated since it includes trig function terms, and they won't all vanish this time.
Let's look at the functions of ##z## we end up with and how they integrate. For ##M^{01}##, there is no change from before: we still have ##z## integrated over ##- Z / 2## to ##Z / 2##, which gives zero. Note that the reason for this is that ##z## is an odd function and is being integrated over an even domain. So we can focus only on the components that are even functions of ##z##; there are three, ##M^{02}##, ##M^{12}##, and ##M^{23}## (which is unchanged from before).
So we need to evaluate two new integrals (plus we have one unchanged from before):
$$
M_{\text{total}}^{02} = - \gamma R \int_{-Z/2}^{Z/2} \cos ( \frac{2 \pi z}{Z} ) = - \gamma R \frac{Z}{2 \pi} \left[ \sin ( \frac{2 \pi z}{Z} ) \right]_{-Z/2}^{Z/2} = 0
$$
$$
M_{\text{total}}^{12} = - \gamma \omega R \int z \sin ( \frac{2 \pi z}{Z} ) = - \gamma \omega R \left[ - \frac{Z}{2 \pi} z \cos ( \frac{2 \pi z}{Z} ) + \frac{Z^2}{4 \pi^2} \sin ( \frac{2 \pi z}{Z} ) \right]_{-Z/2}^{Z/2} = - \gamma \omega R \frac{Z^2}{\pi}
$$
$$
M_{\text{total}}^{23} = \gamma \omega R^2 Z
$$
This is telling us two things. First, since ##M^{02}## vanishes, we don't have a "mass moment" in this frame, which is good because in this frame the cylinder is not translating, only rotating, and a nonzero "mass moment" would imply translation. Second, since ##M^{12}## does
not vanish, the angular momentum is
not solely in the x-y plane; it is partly in the x-z plane as well, at least at time ##t = 0##. In other words, the plane of the angular momentum is
not perpendicular to the axis of rotation.
In other words, the above analysis appears to be saying that the helix motion, considered dynamically, should not be a free motion, since the plane of its angular momentum is not perpendicular to the axis of rotation. If a helix were started with the assumed 4-velocity field, but no further external forces were applied, what should happen is that the axis of rotation should precess (so the 4-velocity field we assumed would not be valid after ##t = 0##). Alternatively, in order to maintain the assumed 4-velocity field over time, external forces would have to be applied to change the angular momentum vector in the right way with time in order to keep the axis of rotation constant. (If we evaluate the above integrals for arbitrary ##t##, we will see that indeed the plane of the angular momentum changes--in general it has components in both the x-z and y-z planes, as well as the x-y plane.)
I'll save for a follow-up post the question of whether we can, as maline suggested, construct a helix motion, with an axis of rotation as assumed here, that is a valid free motion by altering the mass distribution.