For steady uniform-density inviscid flow with no body force, the Euler equations read . Dotting with gives
Thus the Bernoulli equation states that is constant along each streamline; the constants need not be the same on unrelated streamlines.
In the slowly varying tube approximation, mass conservation gives , so . The upstream Bernoulli constant and the wall pressure law give
Subtracting the internal radius obtains
This is choking by wall thickness in an elastic tube. The function tends to as either or , and . Its derivative is
It is positive before and negative afterwards, so the unique maximum is
The maximum is nonnegative because the arithmetic-geometric mean inequality gives ; it is zero only at . If any prescribed thickness exceeds , no positive velocity can satisfy the mass/Bernoulli conditions there, so no flow of this assumed form is possible. Equality is the double-root critical case.
For each , strict monotonicity on and , together with the two negative-infinite limits, gives exactly two positive roots. The upstream condition is as . Therefore
For , the upstream value lies on the rising branch; for , it lies on the falling branch. Smooth continuation preserves this choice because the branches meet only at , which is excluded by the strict bound. At the upstream state is already critical: , so the requirement cannot hold, and any positive wall thickness is incompatible with the approximation. With the critical root is .
Figure 1.
Velocity branches and critical wall thickness for steady flow through an elastic tube
. Details.
The graph shows the unique maximum and the upstream point on the three parameter regimes. Only the portion with represents nonnegative wall thickness. The vertical maximum line separates the two roots when the prescribed thickness lies strictly below the maximum.