Daniel B. answered 02/17/24
A retired computer professional to teach math, physics
Let
p0 = 1.013×105 Pa be atmospheric pressure,
ρ = 1000 kg/m³ be the density of water,
d1 = 3.2 cm be the diameter of the first pipe,
v1 = 5.4 m/s be the speed of the water in the first pipe,
p1 = 1.7 atm + p0 = 2.736×105 Pa be absolute pressure in the first pipe,
d2 = 2.1 cm be the diameter of the second pipe,
v2 (unknown) be the speed of the water in the second pipe,
p2 (to be calculated) be absolute pressure in the second pipe.
In the absence of any information to the contrary, I will make the following assumptions:
Assumption 1) The pipes are concentric.
That implies that (on average) water does not need to flow higher of lower
when passing from the first pipe to the second.
Assumption 2) There is no heat transfer anywhere.
You can solve this problem by conservation of mass and energy:
The amount of water flowing each second must have the same mass and energy
in both pipes.
Conservation of mass:
The volume of water passing through the first pipe each second is
V1 = π(d1/2)²v1
And through the second pipe
V2 = π(d2/2)²v2
Assuming that water is non-compressible (as we were given only one density number),
we must have V1 = V2:
π(d1/2)²v1 = π(d2/2)²v2
From that
v2 = (d1/d2)²v1
Conservation of energy:
Let m = V1ρ be the mass of water passing through the first pipe each second
(which is the same as the mass passing through the second pipe.)
The water in the first pipe has the following kinds of energy:
- Kinetic energy = mv1²/2,
- Potential energy = PE -- an arbitrary constant, which by assumption 1) is the same for both pipes,
- Pressure energy = p1V1
- Internal energy = U -- an arbitrary constant, which by Assumptions 2) must be the same in both pipes.
The analogous energy quantities exist for the second pipe.
Conservation of energy then becomes
mv1²/2 + PE + p1V1 + U = mv2²/2 + PE + p2V2 + U
Thus
p2 = ((v1² - v2²)m/2 + p1V1)/V2
= (v1² - v2²)m/2V2 + p1V1/V2
= (v1² - ((d1/d2)²v1)²)ρ/2 + p1
= v1²(1 - (d1/d2)4)ρ/2 + p1
Now we can substitute actual numbers, making sure that the units are consistent.
That implies that p1 must be absolute pressure expressed in Pa.
p2 = 5.4²×(1 - (3.2/2.1)4)×1000/2 + 2.736×105 = 2.0957×105 Pa
To get gauge pressure, we need to subtract atmospheric pressure:
2.0957×105 - 1.013×105 = 1.0827×105 Pa = 1.07 atm