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malfutka [58]
3 years ago
12

How to build a robot

Engineering
1 answer:
Anuta_ua [19.1K]3 years ago
7 0
Seriously? Ok

first, get some good quality metal, preferably aluminum, if you want to avoid rust.

build in the the shape of a robot, you can use a doll to help you if you are a beginner, but feel free to shape it the a Star Wars Character!

create an AI (now you said robot not AI) and fix everything up.
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Air enters a compressor operating at steady state with pressure of 90 kPa, at a temperature of 350 K, and a volumetric flow rate
natita [175]

Answer:

T_{out} = 457.921\,K

Explanation:

Before determining the exit temperature of air, it is required to find the specific enthalpy at outlet by using the First Law of Thermodynamics:

-\dot Q_{out} + \dot W_{un} + \dot m \cdot (h_{in}-h_{out})=0

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An ideal gas observes the following mathematical model:

P\cdot V = n\cdot R_{u}\cdot T

Where:

P - Absolute pressure, in kilopascals.

V - Volume, in cubic meters.

n - Quantity of moles, in kilomole.

R_{u} - Ideal gas universal constant, in \frac{kPa\cdot m^{3}}{kmole\cdot K}.

T - Absolute temperature, in kelvin.

The previous equation is re-arranged in order to calculate specific volume at inlet:

P\cdot V = \frac{m}{M}\cdot R_{u}\cdot T

\nu = \frac{R_{u}\cdot T}{P\cdot M}

\nu_{in} = \frac{(8.314\,\frac{kPa\cdot m^{3}}{kmol\cdot K} )\cdot (350\,K)}{(90\,kPa)\cdot (28.97\,\frac{kg}{kmol} )}

\nu_{in} = 1.116\,\frac{m^{3}}{kg}

The mass flow is:

\dot m = \frac{\dot V}{\nu_{in}}

\dot m = \frac{0.6\,\frac{m^{3}}{s} }{1.116\,\frac{m^{3}}{kg} }

\dot m = 0.538\,\frac{kg}{s}

The specific enthalpy in ideal gases depends on temperature exclusively. Then:

h_{in} = 350.49\,\frac{kJ}{kg}

The specific enthalpy at outlet is:

h_{out} = \frac{75\,kW}{0.538\,\frac{kg}{s} }-30\,\frac{kJ}{kg} + 350.49\,\frac{kJ}{kg}

h_{out} = 459.895\,\frac{kJ}{kg}

The exit temperature of air is:

T_{out} = 457.921\,K

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3 years ago
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he ventilating fan of the bathroom of a building has a volume flow rate of 28 L/s and runs continuously. If the density of air i
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Answer:

\Delta m = 2903.04 kg

Explanation:

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Answer:

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Explanation:

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