Assignment 5 phy2

course PHY202

xܓۉIzassignment #005

005. `query 4

Physics II

09-14-2008

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10:35:38

query introset plug of water from cylinder given gauge pressure, c-s hole area, length of plug.

Explain how we can determine the velocity of exiting water, given the pressure difference between inside and outside, by considering a plug of known cross-sectional area and length?

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RESPONSE -->

THe work on the plug = force * distance = ('dp*A) *L. 'dp is the pressure difference, L is the length, A is the cross-sectional area.

We can then find the mass of the plug by m= 'rho *L*A. WHere rho is the density.

We can determine KE when the water is at rest by KE = .5mv^2 = work done on plug. Where mis the mass and v is the exit velocity. Using algebra we can find that .5mv^2 = 'dP*A*L then we can substitute to obtain .5 'rho*L*A*v^2 = 'dP *A*L. We can then solve for v to get v = 'squareroot(2*dP*A*L/ ('rho*L*A)) = 'sqrt(2'dP/'rho).

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10:40:20

prin phy problem 10.3. Mass of air in room 4.8 m x 3.8 m x 2.8 m.

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RESPONSE -->

4.8m * 3.8m * 2.8m = 51.072m^3

51.072m^3 * 1.29kg/m^3 = 65.88kg

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10:40:45

The density of air at common atmospheric temperature and pressure it about 1.3 kg / m^3.

The volume of the room is 4.8 m * 3.8 m * 2.8 m = 51 m^3, approximately. The mass of the air in this room is therefore

mass = density * volume = 1.3 kg / m^3 * 51 m^3 = 66 kg, approximately.

This is a medium-sized room, and the mass is close to the average mass of a medium-sized person.

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RESPONSE -->

ok

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11:01:07

prin phy problem 10.8. Difference in blood pressure between head and feet of 1.60 m tell person.

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RESPONSE -->

'dP = pgh = (1.05X10^3 kg/m^3) * (9.8m/s^2) * 1.60m = 16464N/m^2

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11:01:50

The density of blood is close to that of water, 1000 kg / m^3. So the pressure difference corresponding to a height difference of 1.6 m is

pressure difference = rho g h = 1000 kg/m^3 * 9.80 m/s^2 * 1.60 m = 15600 kg / ( m s^2) = 15600 (kg m / s^2) / m^2 = 15600 N / m^2, or 15600 Pascals.

1 mm of mercury is 133 Pascals, so 15,600 Pa = 15,600 Pa * ( 1 mm of Hg / 133 Pa) = 117 mm of mercury.

Blood pressures are measured in mm of mercury; e.g. a blood pressure of 120 / 70 stands for a systolic pressure of 120 mm of mercury and a diastolic pressure of 70 mm of mercury.

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RESPONSE -->

I did not convert to mm Hg

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11:22:59

prin phy and gen phy 10.25 spherical balloon rad 7.35 m total mass 930 kg, Helium => what buoyant force

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RESPONSE -->

920kg

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11:26:18

** The volume of the balloon is about 4/3 pi r^3 = 1660 cubic meters and mass of air displaced is about 1.3 kg / m^3 * 1660 m^3 = 2160 kg.

The buoyant force is equal in magnitude to the force of gravity on the displaced air, or about 2160 kg * 9.8 m/s^2 = 20500 Newtons, approx.. If the total mass of the balloon, including helium, is 930 kg then the net force is about

buoyant force - weight = 20,500 N - 9100 N = 11,400 N

If the 930 kg doesn't include the helium we have to account also for the force of gravity on its mass. At about .18 kg/m^3 the 1660 m^3 of helium will have mass about 300 kg on which gravity exerts an approximate force of 2900 N, so the net force on the balloon would be around 11,400 N - 2900 N = 8500 N approx.

The mass that can be supported by this force is m = F / g = 8500 N / (9.8 m/s^2) = 870 kg, approx.. **

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RESPONSE -->

ok

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11:26:27

univ 14.51 (14.55 10th edition) U tube with Hg, 15 cm water added, pressure at interface, vert separation of top of water and top of Hg where exposed to atmosphere.

Give your solution to this problem.

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RESPONSE -->

ok

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11:26:32

** At the interface the pressure is that of the atmosphere plus 15 cm of water, or 1 atm + 1000 kg/m^3 * 9.8 m/s^2 * .15 m = 1 atm + 1470 Pa.

The 15 cm of water above the water-mercury interface must be balanced by the mercury above this level on the other side. Since mercury is 13.6 times denser than water there must therefore be 15 cm / (13.6) = 1.1 cm of mercury above this level on the other side. This leaves the top of the water column at 15 cm - 1.1 cm = 13.9 cm above the mercury-air interface.

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Here's an alternative solution using Bernoulli's equation, somewhat more rigorous and giving a broader context to the solution:

Comparing the interface between mercury and atmosphere with the interface between mercury and water we see that the pressure difference is 1470 Pa. Since velocity is zero we have P1 + rho g y1 = P2 + rho g y2, or

rho g (y1 - y2) = P2 - P1 = 1470 Pa.

Thus altitude difference between these two points is

y1 - y2 = 1470 Pa / (rho g) = 1470 Pa / (13600 kg/m^2 * 9.8 m/s^2) = .011 m approx. or about 1.1 cm.

The top of the mercury column exposed to air is thus 1.1 cm higher than the water-mercury interface. Since there are 15 cm of water above this interface the top of the water column is

15 cm - 1.1 cm = 13.9 cm

higher than the top of the mercury column.

NOTE BRIEF SOLN BY STUDENT:

Using Bernoullis Equation we come to:

'rho*g*y1='rho*g*y2

1*10^3*9.8*.15 =13.6*10^3*9.8*y2

y2=.011 m

h=y1-y2

h=.15-.011=.139m

h=13.9cm. **

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RESPONSE -->

ok

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&#This looks good. Let me know if you have any questions. &#