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kicyunya [14]
3 years ago
15

A small vehicle is powered by a pulsejet. The available net thrust is 6000 N and the traveling speed is 200 km/hr. The gases lea

ve the engine with an average velocity (Ve) of 360 m/s Assume pressure equilibrium exists at the outlet plane and the fuel to air ratio is 0.06.
a. Compute the mass flow rate required
b. Calculate the inlet area (assume To is 16 °C and Po is one atmosphere)
C. Calculate the thrust power
d. Calculate the propulsive efficiency
Engineering
1 answer:
kumpel [21]3 years ago
4 0

Answer:

a) The mass flow rate is 19.71 kg/s

b) The inlet area is 0.41 m²

c) The thrust power is 333.31 kW

d) The propulsive efficiency is 26.7%

Explanation:

Please look at the solution in the attached Word file.

Download docx
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Answer:

C

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So

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Answer:

\omega_y,\omega_x,\omega_Z  all are zero.

Explanation:

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Rotationality of fluid is given by \omega

\frac{\partial v}{\partial x}-\frac{\partial u}{\partial y}=\omega_Z

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So \omega_y=0

Like this all \omega_y,\omega_x,\omega_Z all are zero.

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A horizontal curve is being designed through mountainous terrain for a four-lane road with lanes that are 10 ft wide. The centra
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our answer is attached below

Explanation:

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Answer: you forgot to add the rest of the Questions in.

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