Class 11th

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New answer posted

8 months ago

0 Follower 2 Views

V
Vishal Baghel

Contributor-Level 10

The area of the wing of the plane, A = 2 *25m2 = 50 m2

Speed of air over the lower wing, V1 = 180 km/h = 50 m/s

Speed of air over the upper wing, V2 = 234 km/h = 65 m/s

Density of air, ρ = 1 kg/ m3

Let us assume, pressure over the lower wing = P1 and pressure over the upper wing = P2

The upward force on the plane can be obtained using Bernoulli's equation:

On lower wing= P1 + 12ρV12 , On upper wing = P2 + 12ρV22

From equilibrium of momentum

P1 + 12ρV12 = P2 + 12ρV22

P1 - P2)=12ρ(V22-V12 )

The net upward force = ( P1 - P2)A = 12ρ(V22-V12 ) *A

=&nbs

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New answer posted

8 months ago

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V
Vishal Baghel

Contributor-Level 10

Radius of the artery, r = 2 *10-3 m

Diameter of the artery, d = 4 *10-3 m

Viscosity of blood, η = 2.084 *10-3 Pa-s

Density of the blood, ρ = 1.06 *103 kg/ m3

Reynolds's number for laminar flow, Re = 2000

The largest velocity is given by the relation: Vavg = Reηρd

2000*2.084*10-31.06*103*4*10-3 = 0.983 m/s

Flow rate is given by the relation:

R = πr2Vavg = 3.1416 *(2*10-3)2*0.983 = 1.235 *10-5 m3 /s

New answer posted

8 months ago

0 Follower 2 Views

V
Vishal Baghel

Contributor-Level 10

Diameter of the artery, d = 2 *10-3 m

Viscosity of the blood,  η = 2.084 *10-3 Pa-s

Density of the blood,  ρ = 1.06 *103 kg/ m3

Reynolds's number for laminar flow,  Re = 2000

Vavg = Reηρd = 2000*2.084*10-31.06*103*2*10-3 = 1.966 m/s

As the fluid velocity increases, the dissipative forces become more important. This is because of the rise of turbulence. Turbulent flow causes dissipative loss in a fluid.

New answer posted

8 months ago

0 Follower 2 Views

V
Vishal Baghel

Contributor-Level 10

Gauge pressure, P = 2000 Pa

Density of whole blood,  ρ = 1.06 *103 kg/ m3

Acceleration due to gravity, g = 9.8 m/s

Let the height of the blood container = h

Pressure on the blood container P = ρgh

By equating, we get h = (2000)/ ( 1.06 *103*9.8) = 0.1925m

New answer posted

8 months ago

0 Follower 1 View

V
Vishal Baghel

Contributor-Level 10

Two vessels, having the same base area, will have identical force and equal pressure acting on their common base area. Since the shapes of the two vessels are different, the force exerted on the sides of the vessels has non-zero vertical components.

When these vertical components are added, the total force on one vessel comes out to be more than on the other vessel. Hence, when these vessels are filled with water to the same height, they give different readings on the weighing scale.

New answer posted

8 months ago

0 Follower 9 Views

V
Vishal Baghel

Contributor-Level 10

Atmospheric pressure,  P0 = 76 cm of Hg

For figure (a)

Difference between the levels of mercury in the two limbs gives gauge pressure

Hence, gauge pressure = 20 cm of Hg

Absolute pressure = Atmospheric pressure + Gauge pressure = 76 + 20 = 96 cm of Hg

For figure (b),

Difference between the levels of mercury in the two limbs gives gauge pressure

Hence, gauge pressure = - 18 cm of Hg

Absolute pressure = Atmospheric pressure + Gauge pressure = 76 - 18 = 58 cm of Hg

When 13.6 cm of water is poured into the right limb of figure (b)

Relative density of mercury = 13.6

Hence, a column of 13.6 cm of water is equivalent to 1 cm of Mercury.

Let h be

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New answer posted

8 months ago

0 Follower 2 Views

P
Payal Gupta

Contributor-Level 10

11.22

The fusion and boiling points are given by the intersection point where this parallel line cuts the fusion and vaporization curves. It departs from ideal gas behavior as pressure increases.

(a) At 1 atm pressure and at – 60 °C, it lies left of -56.6 ? (triple point O). Hence, it lies in the region of vapour and solid phases. Thus,  CO2  condenses into solid state directly, without going through liquid phases.

(b) At 4 atm pressure,  CO2 lies below 5.11 atm (triple point O). Hence it lies in the region of vaporous and solid phases. Thus, CO2 condenses into solid state directly, without going through liquid state.

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New answer posted

8 months ago

0 Follower 4 Views

V
Vishal Baghel

Contributor-Level 10

Base area of the given tank, A = 1.0 m2

Area of the hinged door, a = 20 cm2 = 20 *10-4 m2

Density of water, ρ1 = 103 kg/ m3

Density of acid, ρ2 = 1.7 *103 kg/ m3

Height of the water column, h1 = 4 m

Height of the acid column, h2 = 4 m

Acceleration due to gravity, g = 9.8 m/ s2

The pressure due to Water column, P1 = ρ1gh1 = 103*9.8*4 = 3.92 *104 Pa

The pressure due to Acid column, P2 = ρ2gh2 = 1.7 *103*9.8*4 = 6.64 *104 Pa

Pressure difference between two columns ΔP = P2 - P1 = 2.774 *104 Pa

Force exerted on the small hi

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New answer posted

8 months ago

0 Follower 1 View

V
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

8 months ago

0 Follower 7 Views

P
Payal Gupta

Contributor-Level 10

11.21 

(a) The P-T phase diagram for CO2 is shown here. O is the triple point of the CO2 phase diagram. This means that at the temperature and pressure corresponding to this point, the solid, liquid and vaporous phases of CO2 exists in equilibrium.

(b) The fusion and the boiling points of CO2 decreases with a decrease in pressure.

(c) The critical temperature and critical pressure of CO2 are 31 ? 72.9 atm respectively. Even if it is compressed to a pressure greater than 72.9 atm, CO2 will not liquefy above the critical temperature.

(d) It can be concluded from the P-T phase diagram of CO2 that:

CO2 is gaseous at -70 ? , under 1 atm pr

...more

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