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Only the Turned Flux Has Leverage

Irodov 1.328DifficultyDifficulty 4 of 5UniquenessUniqueness 4 of 5

Problem Irodov 1.328

A large tank of water drains through a tube of uniform inside radius r=0.50r = 0.50 cm attached to its side. The tube runs horizontally away from the tank for a length l=22l = 22 cm, then turns through a right angle and runs vertically downward, and the water leaves through its open lower end. The volume flow rate is Q=0.50Q = 0.50 liters per second. Let OO be the point where the tube meets the tank, at the upstream end of the horizontal run. Find the moment about OO of the reaction forces that the flowing water exerts on the walls of the tube.

Water leaves the tank along a horizontal run of length l, turns through a right angle, and falls from the open lower end with speed v. Here l runs from the joint O to the vertical run's axis.

Water leaves the tank along a horizontal run of length ll, turns through a right angle, and falls from the open lower end with speed vv. Here ll runs from the joint OO to the vertical run’s axis.

Given
  • r=0.50r = 0.50 cm
  • l=22l = 22 cm
  • Q=0.50Q = 0.50 liters/s
  • ρ=1.00×103\rho = 1.00\times10^3 kg/m3^3
Find
Find NN, the moment about OO of the reaction forces the flowing water exerts on the tube’s walls

Solution

Step 1Speed of the water in the tube

The bore is the same everywhere along the tube, so the same volume crosses every section each second and one continuity statement fixes the speed.

Q=Sv=πr2v.Q = Sv = \pi r^2 v.
v=Qπr2v = \dfrac{Q}{\pi r^2}
(1)
The control volume: the water in the tube between the inlet at O and the open outlet. The incoming flux ρ Q v_1 lies on a line through O; the outgoing flux ρ Q v_2 lies a distance l away.

The control volume: the water in the tube between the inlet at OO and the open outlet. The incoming flux ρQv1\rho Q\vect v_1 lies on a line through OO; the outgoing flux ρQv2\rho Q\vect v_2 lies a distance ll away.

Step 2Moment-of-momentum balance for the water in the tube

Take as control volume all the water between the inlet section at OO and the open outlet, and write the moment-of-momentum theorem about OO for it: the total moment of the external forces equals the rate at which angular momentum accumulates inside plus the rate at which it is carried out through the boundary.

∑MO=∂∂t∫V(r×ρu) dV+∮S(r×u) ρ u⋅dS,∑MO=ρQ (r2×v2)−ρQ (r1×v1).(2) \begin{aligned} \sum\vect M_O &= \frac{\partial}{\partial t}\int_V (\vect r\times\rho\vect u)\,dV + \oint_S (\vect r\times\vect u)\,\rho\,\vect u\cdot d\vect S, \\ \sum\vect M_O &= \rho Q\,(\vect r_2\times\vect v_2) - \rho Q\,(\vect r_1\times\vect v_1). \end{aligned} \tag{2}

The first term drops because the flow is steady, and the surface integral collects nothing along the walls, where the water does not cross the boundary, leaving only the two end sections, each carrying mass at the rate ρQ\rho Q with the uniform velocity of its own section.

Step 3Only the outgoing flux carries an arm about OO

Put the origin at OO, with i\vect i along the horizontal run pointing away from the tank and j\vect j vertically upward, so that k=i×j\vect k = \vect i\times\vect j points out of the page. The inlet section sits at OO itself; the outlet sits a distance ll along i\vect i and a distance hh below, hh being the length of the vertical run.

r1=0,v1=v i,r2=l i−h j,v2=−v j.\begin{align*}\vect r_1 &= \vect 0, & \vect v_1 &= v\,\vect i, \\ \vect r_2 &= l\,\vect i - h\,\vect j, & \vect v_2 &= -v\,\vect j.\end{align*}

Forming the two cross products term by term gives the angular momentum carried in and out.

r1×v1=0,r2×v2=(l i−h j)×(−v j)=−lv (i×j)+hv (j×j)=−lv k.\begin{align*}\vect r_1\times\vect v_1 &= \vect 0, \\ \vect r_2\times\vect v_2 &= (l\,\vect i - h\,\vect j)\times(-v\,\vect j) \\ &= -lv\,(\vect i\times\vect j) + hv\,(\vect j\times\vect j) \\ &= -lv\,\vect k.\end{align*}

Substituting both into (2),

∑MO=−ρQlv k.\sum\vect M_O = -\rho Q l v\,\vect k.
Step 4The wall reaction is the only moment left

The external forces on the water in the control volume come in three kinds: the pressure on the two end sections, the water’s own weight, and the push of the walls. Measuring pressures from atmospheric, the force on the inlet section is uniform over that section, so its resultant passes through OO and has no arm, and the open outlet carries no such force at all; the weight contributes a static moment that contains no QQ. What survives is the moment the walls exert on the water. Set aside, with the weight, the static part of that wall moment which balances it, and write Mw\vect M_w for the flow-borne part that remains; the balance and Newton’s third law then read

Mw=−ρQlv k,N=−Mw.\begin{align*}\vect M_w &= -\rho Q l v\,\vect k, \\ \vect N &= -\vect M_w.\end{align*}
N=ρQlv k\vect N = \rho Q l v\,\vect k
(3)

Out of the page is counterclockwise in the figure’s plane, so the reaction tends to swing the bent end of the tube upward about OO, which is the tube’s share of turning the stream downward.

Step 5Evaluate

Substituting the speed of (1) into the magnitude of (3), with every quantity converted to SI units and the density of water taken from the tables,

N=(1.00×103)(0.22) (0.50×10−3)2π (0.50×10−2)2 N⋅m.N = (1.00\times10^3)(0.22)\, \frac{(0.50\times10^{-3})^2}{\pi\,(0.50\times10^{-2})^2}\ \text{N}\cdot\text{m}.
N=ρlQ2πr2≈0.70 N⋅mN = \dfrac{\rho l Q^2}{\pi r^2} \approx 0.70\ \text{N}\cdot\text{m}
(4)
Check

The units come out right: (kg/m3)(m)(m3/s)2/m2=kg⋅m2/s2(\text{kg/m}^3)(\text{m})(\text{m}^3/\text{s})^2/\text{m}^2 = \text{kg}\cdot\text{m}^2/\text{s}^2, a newton meter. The number checks by a second route as well. The stream is turned from horizontal to vertical at the bend, so the vertical part of the force the water delivers there is ρQv\rho Qv, which is 3.23.2 N here, and its arm about OO is the whole horizontal run of 2222 cm; the product of those two is 0.700.70 N⋅\cdotm, the answer above.

Remark

The answer cannot be separated from the point it is taken about, and among the points of the tube itself the bend is the one where it collapses. Seen from the corner, the incoming momentum flux runs along the horizontal leg and the outgoing flux runs along the vertical leg, so each position vector is parallel to its own velocity, both cross products vanish, and the elbow feels a force but exerts no moment about itself. The whole of NN is therefore the arm ll that the tank joint lends to the vertical, turned part of that force, while the horizontal part acts along the tube’s own axis, straight through OO, and contributes nothing at all. Away from the tube the vanishing is not unique: the dynamic moment is zero at every point of the resultant’s own line of action, the 4545 degree line through the corner along which ρQv(i+j)\rho Qv(\vect i+\vect j) acts, and the bend is simply where that line crosses the tube. Both statements lean on this particular geometry, the outlet directly below the bend and the inlet flux along the horizontal axis; tilt either leg and each of them has to be redrawn.