Mechanical Properties of Fluids

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7 months ago

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Vishal Baghel

Contributor-Level 10

Soap bubble radius, r = 5.0 mm = 5 *10-3 m

Surface tension of the soap bubble, S = 2.50 *10-2 N/m

Relative density of soap solution = 1.20, hence density of soap solution,  ?  = 1.2 *103 Kg/ m3

Air bubble formed at a depth, h = 40 cm = 0.4 m

1 atmospheric pressure = 1.01 *105 Pa

Acceleration due to gravity, g = 9.8 m/ s2

We know, the excess pressure inside the soap bubble is given by the relation:

P = 4Sr = 4*2.50*10-25*10-3 Pa = 20 Pa

Hence, the excess pressure inside the air bubble is given by the relation, P' = 2Sr = 10 Pa

At a depth of h, the total pressure inside the air bubble = Atmospheric press

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New answer posted

7 months ago

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Vishal Baghel

Contributor-Level 10

Radius of the mercury droplet, r = 3.00 mm = 3 *10-3 m

Surface tension, S = 4.65 *10-1 N/m

Atmospheric pressure,  Po = 1.01 *105 Pa

Total pressure inside the mercury drop = Excess pressure inside mercury + Atmospheric pressure

2Sr + Po = 2*4.65*10-13*10-3 + 1.01 *105 = 1.01310 *105 Pa

Excess pressure inside mercury = 2Sr = 2*4.65*10-13*10-3 = 310 Pa

New answer posted

7 months ago

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Vishal Baghel

Contributor-Level 10

Let us take the case (a):

The length of the liquid film supported by the weight, l = 40 cm = 0.4 m

The weight supported by the film, W = 4.5 *10-2 N

Since a liquid film has two free surfaces,

Surface tension = W2l = 4.5*10-22*0.4 = 5.625 *10-2 N/m

In all 3 figures, the liquid is the same, temperature is also the same. Hence the surface tension in (b) and (c) are also going to be the same, with the value of 5.625 *10-2 N/m and weight supported in each case is also going to be the same, since length of the film is same.

New answer posted

7 months ago

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Vishal Baghel

Contributor-Level 10

The weight that the soap film supports, W = 1.5 *10-2 N

Length of the slider, l = 30 cm = 0.3 m

A soap film has two free surfaces, hence total length = 2l = 0.6 m

Surface tension, S= Forces/Weight2l = 1.5*10-22*0.3 = 2.5 *10-2 N/m

New answer posted

7 months ago

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Vishal Baghel

Contributor-Level 10

Area of cross-section of the spray pump, A1 = 8 cm2 = 8 *10-4 m2

Number of holes, n = 40

Diameter of each hole, d = 1 mm = 1 *10-3 m

Radius of each hole, r = d/2 = 0.5 *10-3 m

Area of cross-section of each hole, a = πr2 = π(0.5*10-3)2

Total area of 40 holes, A2 = 40 π*(0.5*10-3)2 = 3.14 *10-5 m2

Speed of liquid inside the tube, V1 = 1.5 m/min = 0.025 m/s

Speed of ejection of liquid = V2

According to law of continuity, we have A1V1 = A2V2 or V2=A1V1A2 = 8*10-4*0.0253.14*10-5

= 0.637 m/s

New answer posted

7 months ago

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Vishal Baghel

Contributor-Level 10

Take the case given in figure (b)

A1 = Area of pipe 1,  A2 = Area of pipe 2,  V1 = Speed of fluid in pipe 1,  V2 = Speed of fluid in pipe 2

From the law of continuity, we have

A1V1 = A2V2

When the area of cross-section in the middle of the venturimeter is small, the speed of the flow of liquid through this part is more. According to Bernoulli's principle, if speed is more, the pressure is less. Pressure is directly proportional to height, hence the level of water in pipe 2 is less. Therefore, figure (a) is not possible.

New answer posted

7 months ago

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Vishal Baghel

Contributor-Level 10

Speed of the wind on the upper surface of the wing, V1 = 70 m/s

Speed of the wind on the lower surface of the wing, V2 = 63 m/s

Area of the wing, A = 2.5 m2

Density of air, ρ = 1.3 kg/ m3

According to Bernoulli's theorem, we have the relation:

P1 + 12ρV12 = P2 + 12ρV22

P2 - P1 )= 12ρ(V12 - V22) , where P1 = pressure on the upper surface of the wing and P2 - pressure on the lower surface of the wing

The pressure difference provides lift to the aeroplane

Lift on the wing = ( P2 - P1 )A = 12ρ(V12 - V22) A = 12*1.3*(702 - 632)*2.5 N =

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New answer posted

7 months ago

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Vishal Baghel

Contributor-Level 10

Length of the horizontal tube, l = 1.5 m

Radius of the tube, r = 1 cm = 0.01 m

Diameter of the tube, d = 2r = 0.02m

Glycerine mass flow rate, M = 4 *10-3 kg/s

Density of glycerine, ρ = 1.3 *103 kg

Viscosity of glycerine, η = 0.83 Pa-s

Now, volume of glycerine flowing per sec V = Mρ = 4*10-31.3*103 m3 /s = 3.08 *10-6 m3 /s

According to Poiseville's formula, we know the flow rate

V = π*p*r48*η*l where p is the pressure difference between two ends of the tube

p = V*8*η*lπ*r4 = 3.08*10-6*8*0.83*1.5π*(0.01)4 = 976.47 Pa

Reynolds's number is given by the relation

Re = 4ρVπdη = 4*1.3*103*3.08*10-63.1416*0.02*0.83 = 0.3

Since the Reynolds's number is 0

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New answer posted

7 months ago

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Vishal Baghel

Contributor-Level 10

It does not matter if one uses gauge pressure, instead of absolute pressure while applying Bernoulli's equation. There should be significantly different atmospheric pressures, where Bernoulli's equation is applied.

New answer posted

7 months ago

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Vishal Baghel

Contributor-Level 10

No, Bernoulli's equation cannot be used to describe the flow of water through a rapid in a river. In rapid, the flow is turbulent whereas Bernoulli's equation is applicable for laminar flow only.

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