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melomori [17]
3 years ago
10

Explain what the ancient Romans did to solve the problem in the following scenario.

Engineering
1 answer:
Nonamiya [84]3 years ago
6 0

Answer:

They moved fresh water around their vast empire with aqueducts and canals.

Explanation:

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B because thermal has to do with temperature and it’s the amount of kinetic and potential energy in and object
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Explain when it is appropriate to use Tier II?
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Special considerations must be given to systems using liquid hydrogen for fuel because of: A. Liquid hydrogen's low density B. L
vitfil [10]

Answer:

D.All of the above

Explanation:

Properties of hydrogen:

1.It is lighter than air.It has density about 0.089 g/L.

2.Hydrogen  rapidly change from liquid state to gas,so special protection is required to protect it.

3.It is highly flammable gas.

4.Liquid form of hydrogen exits at -432 F .This is very low temperature so special protection requires to keep it in liquid form.          

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3 years ago
I need help!!!!!!!!!
katovenus [111]

Answer:

buy a new one

Explanation:

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8 0
3 years ago
A ramjet operates by taking in air at the inlet, providing fuel for combustion, and exhausting the hot air through the exit. Th
UNO [17]

Answer:

15300 N

Explanation:

\rho_i = Density of air at inlet

\dfrac{m}{t} = Mass flow rate = 60 kg/s

v_i = Inlet velocity = 225 m/s

\rho_o = Density of gas at outlet = 0.25\ \text{kg/m}^3

A_i = Inlet area

A_o = Outlet area = 0.5\ \text{m}^2

Since mass flow rate is the same in the inlet and outlet we have

\rho_iv_iA_i=\rho_ov_oA_o\\\Rightarrow v_o=\dfrac{\dfrac{m}{t}}{\rho_oA_o}\\\Rightarrow v_o=\dfrac{60}{0.25\times 0.5}\\\Rightarrow v_o=480\ \text{m/s}

Thrust is given by

F=\dfrac{m}{t}(v_o-v_i)\\\Rightarrow F=60\times (480-225)\\\Rightarrow F=15300\ \text{N}

The thrust generated is 15300 N.

8 0
3 years ago
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