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Question 2) In order to test a jet engine at sea level, it is aimed to design a static thrust stand for the given following conditions: Inlet: Velocity= 200 m/s, Area= 1.2 m², Static absolute pressure= 75 kPa, Static temperature= 272 K Exit: Velocity= 600 m/s, Static gage pressure= 0 kPa a) Using the control volume in the figure to the right, calculate the nominal thrust level to design this stand for. b) Rewrite the equation of conservation of momentum if another control volume is selected for the analysis as shown to the right. Show how it simplifies down to the equation you have used in part (a). Explain why. c) In which direction would the engine move if it was not mounted onto the thrust stand?

          Question 2) In order to test a jet engine at sea level, it is aimed to design a static thrust stand for the
given following conditions:
Inlet: Velocity= 200 m/s, Area= 1.2 m², Static absolute pressure= 75 kPa, Static temperature= 272 K
Exit: Velocity= 600 m/s, Static gage pressure= 0 kPa
a) Using the control volume in the figure to the right,
calculate the nominal thrust level to design this stand for.
b) Rewrite the equation of conservation of momentum if another control volume is
selected for the analysis as shown to the right. Show how it simplifies down to the
equation you have used in part (a). Explain why.
c) In which direction would the engine move if it was not mounted onto the thrust stand?
        
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Question 2) In order to test a jet engine at sea level, it is aimed to design a static thrust stand for the
given following conditions:
Inlet: Velocity= 200 m/s, Area= 1.2 m², Static absolute pressure= 75 kPa, Static temperature= 272 K
Exit: Velocity= 600 m/s, Static gage pressure= 0 kPa
a) Using the control volume in the figure to the right,
calculate the nominal thrust level to design this stand for.
b) Rewrite the equation of conservation of momentum if another control volume is
selected for the analysis as shown to the right. Show how it simplifies down to the
equation you have used in part (a). Explain why.
c) In which direction would the engine move if it was not mounted onto the thrust stand?

Added by Francisco W.

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University Physics with Modern Physics
University Physics with Modern Physics
Hugh D. Young 14th Edition
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Transcript

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00:01 In this question we have given one jet engine and we need to find the normal thrust level to design the stand we have given the velocity that is equal to 200 meter per seconds then we have given pressure 1 that is equal to 76 kilos pascal we have given v2 that is equal to 600 meter per seconds right and p1 in gorge will be equal to minus 26 325 gorge then we have given p2 that is equal to zero only right for calculating the mass ms will be equal to row 1 v1 a 1 that will be equal to row 1 is nothing but 0 .96 multiply by v1 that is equal to 200 multiply by a 1 that is nothing but 1 .2 from here the value of ms will be equal to to 230 .4 kilogram per seconds...
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