At the exhaust of a turboject engine the nozzle is operating steadily and heat loss is assumed negligible. If the specific enthalpy of fluid and velocity of fluid at the inlet are 3140 kJ/kg and 238 km/hr respectively. At the exit the specific enthalpy of fluid is 2514 J/kg. Calculate the exit area (in mm2)of the nozzle when the specific volume at the nozzle exit is 0.64 m³/kg at the inlet area of 0.21 m² and the specific volume at the inlet is 0.34 m³/kg. You do not need to include the unit for this question. Calculate answer to 3 d.p.
At the exhaust of a turboject engine the nozzle is operating steadily and heat loss is assumed negligible. If the specific enthalpy of fluid and velocity of fluid at the inlet are 3140 kJ/kg and 238 km/hr respectively. At the exit the specific enthalpy of fluid is 2514 J/kg. Calculate the exit area (in mm2)of the nozzle when the specific volume at the nozzle exit is 0.64 m³/kg at the inlet area of 0.21 m² and the specific volume at the inlet is 0.34 m³/kg. You do not need to include the unit for this question. Calculate answer to 3 d.p.
Refrigeration and Air Conditioning Technology (MindTap Course List)
8th Edition
ISBN:9781305578296
Author:John Tomczyk, Eugene Silberstein, Bill Whitman, Bill Johnson
Publisher:John Tomczyk, Eugene Silberstein, Bill Whitman, Bill Johnson
Chapter40: Typical Operating Conditions
Section: Chapter Questions
Problem 10RQ: The seasonal energy efficiency ratio (SEER) includes the energy used in the _____and _____cycles.
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![At the exhaust of a turboject engine the nozzle is operating steadily and heat loss is assumed
negligible. If the specific enthalpy of fluid and velocity of fluid at the inlet are 3140 kJ/kg and 238 km/hr
respectively. At the exit the specific enthalpy of fluid is 2514 J/kg. Calculate the exit area (in mm
mm²)of the
nozzle when the specific volume at the nozzle exit is 0.64 m³/kg at the inlet area of 0.21 m² and the
specific volume at the inlet is 0.34 m³/kg.
You do not need to include the unit for this question.
Calculate answer to 3 d.p.](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2F4a409a4d-b899-47ef-9488-ccaef97ee1a8%2F72f4c860-f229-4686-9275-40c34db8350a%2F0wyozzj_processed.jpeg&w=3840&q=75)
Transcribed Image Text:At the exhaust of a turboject engine the nozzle is operating steadily and heat loss is assumed
negligible. If the specific enthalpy of fluid and velocity of fluid at the inlet are 3140 kJ/kg and 238 km/hr
respectively. At the exit the specific enthalpy of fluid is 2514 J/kg. Calculate the exit area (in mm
mm²)of the
nozzle when the specific volume at the nozzle exit is 0.64 m³/kg at the inlet area of 0.21 m² and the
specific volume at the inlet is 0.34 m³/kg.
You do not need to include the unit for this question.
Calculate answer to 3 d.p.
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