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laiz
3 months ago
10

A constant-velocity horizontal water jet from a stationary nozzle impinges normally on a vertical flat plate that rides on a nea

rly frictionless track. As the water jet hits the plate, it begins to move due to the water force. As a result, the acceleration will _____.
Physics
1 answer:
Yuliya22 [3.3K]3 months ago
7 0

Answer:

a = ½ ρ A/M   v₁²

Explanation:

This scenario involves fluid mechanics, where a water jet moving at a constant velocity strikes a paddle and during this interaction, the water remains motionless. We will apply Bernoulli's equation, labeling the jet before the impact as index 1 and after the impact as index 2.

           P₁ + ½ ρ v₁² + ρ g h₁ = P₂ + ½ ρ v₂² + ρ g h₂

In this case, the water is at rest post-impact, hence v₂ = 0, while h₁ = h₂ remains horizontal.

          P₁-P₂ = ½ ρ v₁²

         ΔP = ½ ρ v₁²

Now we can use the definition of pressure as a force divided by area.

         F / A = ½ ρ v₁²

         F = 1/2 ρ A v₁²

The density can be defined as

          ρ = m / V

The volume is

           V = A l

           F = ½ m / l v₁²

With the force known, we can focus on the mass accretion of the plate M leading to its acceleration.

         F = M a

         a = F / M

          a = ½ m/M  1/l   v₁²

           

this can also be expressed in terms of the water's density

          a = ½ ρ A/M   v₁²

You might be interested in
At a given point on a horizontal streamline in flowing air, the static pressure is â2.0 psi (i.e., a vacuum) and the velocity is
Softa [3030]
Bernoulli's equation at a point on the streamline is
p/ρ + v²/(2g) = constant
where
p = pressure
v = velocity
ρ = air density, 0.075 lb/ft³ (under standard conditions)
g = 32 ft/s²

Point 1:
p₁ = 2.0 lb/in² = 2*144 = 288 lb/ft²
v₁ = 150 ft/s

Point 2 (stagnation):
The velocity at the stagnation point is zero.

The density stays constant.
Let p₂ denote the pressure at the stagnation location.
Then,
p₂ = ρ(p₁/ρ + v₁²/(2g))
p₂ = (288 lb/ft²) + [(0.075 lb/ft³)*(150 ft/s)²]/[2*(32 ft/s²)
     = 314.37 lb/ft²
     = 314.37/144 = 2.18 lb/in²

Thus, the answer is 2.2 psi

5 0
3 months ago
A supersonic nozzle is also a convergent–divergent duct, which is fed by a large reservoir at the inlet to the nozzle. In the re
Softa [3030]

Answer:

155.38424 K

2.2721 kg/m³

Explanation:

P_1 = Reservoir pressure = 10 atm

T_1 = Reservoir temperature = 300 K

P_2 = Exit pressure = 1 atm

T_2 = Exit temperature

R_s = Specific gas constant = 287 J/kgK

\gamma = Specific heat ratio = 1.4 for air

Assuming isentropic flow

\frac{T_2}{T_1}=\frac{P_2}{P_1}^{\frac{\gamma-1}{\gamma}}\\\Rightarrow T_2=T_1\times \frac{P_2}{P_1}^{\frac{\gamma-1}{\gamma}}\\\Rightarrow T_2=00\times \left(\frac{1}{10}\right)^{\frac{1.4-1}{1.4}}\\\Rightarrow T_2=155.38424\ K

Flow temperature at exit is 155.38424 K

Density at exit can be derived using the ideal gas equation

\rho_2=\frac{P_2}{R_sT_2}\\\Rightarrow \rho=\frac{1\times 101325}{287\times 155.38424}\\\Rightarrow \rho=2.2721\ kg/m^3

Flow density at exit measures 2.2721 kg/m³

4 0
4 months ago
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