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DENIUS [597]
3 years ago
10

The pilot of an airplane reads the altitude 6400 m and the absolute pressure 45 kPa when flying over the city. Calculate the loc

al atmospheric pressure in that city in kPa and in mmHg. Take the densities of air and mercury to be 0.828 kg/m3 and 13600 kg/m3, respectively. Show this using the systematic solution method.
Engineering
1 answer:
garri49 [273]3 years ago
7 0

Answer:

1) The absolute pressure equals = 96.98 kPa

2) Absolute pressure in terms of column of mercury equals 727 mmHg.

Explanation:

using the equation of pressure statics we have

P(h)=P_{surface}-\rho gh...............(i)

Now since it is given that at 6400 meters pressure equals 45 kPa absolute hence from equation 'i' we obtain

P_{surface}=P(h)+\rho gh

Applying values we get

P_{surface}=45\times 10^{3}+0.828\times 9.81\times 6400

P_{surface}=96.98\times 10^{3}Pa=96.98kPa

Now the pressure in terms of head of mercury is given by

h_{Hg}=\frac{P}{\rho _{Hg}\times g}

Applying values we get

h=\frac{96.98\times 10^{3}}{13600\times 9.81}=0.727m=727mmHg

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Explanation:

Hello!

To solve this problem follow the steps below, the complete procedure is in the attached image

1. draw a complete outline of the problem

2. to find the temperature at the turbine exit  use termodinamic tables to find the saturation temperature at 30kPa

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through prior knowledge of two other properties such as pressure and temperature.  

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The 150-lb man sits in the center of the boat, which has a uniform width and a weight per linear foot of 3 lb>ft. Determine t
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Answer:

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Explanation:

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W<em>man</em> = 150 lb

Weight per linear foot of the boat: q = 3 lb/ft

L = 15.00 m

M<em>max</em> = ?

Initially, we have to calculate the Buoyant Force per linear foot (due to the water exerts a uniform distributed load upward on the bottom of the boat):

∑ Fy = 0  (+↑)     ⇒    q'*L - W - q*L = 0

⇒       q' = (W + q*L) / L

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The free body diagram of the boat is shown in the pic.

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