Calculate the Mach number at the exit of the nozzle in Prob. 4.11. 2. A Boeing 747 is cruising at a velocity of250 m/s at a standard altitude of 13 km.
1. Calculate the Mach number at the exit of the nozzle in Prob. 4.11. 2. A Boeing 747 is cruising at a velocity of250 m/s at a standard altitude of 13 km. What is its Mach number? Prob. 4.11. The mass flow of air through a supersonic nozzle is 1.5 lb.,/s. The exit velocity is 1500 , and the reservoir temperature and pressure are 1 000°R and 7 , respectively. Calculate the area of the nozzle exit. For air, Cp = 6000 ft · lb/ (slug)(0R).
What is its Mach number? Prob. 4.11. The mass flow of air through a supersonic nozzle is 1.5 lb.,/s. The exit velocity is 1500 , and the reservoir temperature and pressure are 1 000°R and 7 , respectively. Calculate the area of the nozzle exit. For air, Cp = 6000 ft · lb/ (slug)(0R).
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The post Calculate the Mach number at the exit of the nozzle in Prob. 4.11. 2. A Boeing 747 is cruising at a velocity of250 m/s at a standard altitude of 13 km. appeared first on USA Dissertation Editors.
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