subject
Engineering, 07.08.2019 19:20 skydom654

In an air-standard brayton cycle the air enters the compressor at 100 kpa and 10°c, with a mass flow rate of 6 kg/s. the pressure leaving the compressor is 10 bar and the turbine inlet temperature is 1100°c. for k=1.4, calculate the compressor, turbine, and network as well as the thermal efficiency of the cycle.

ansver
Answers: 2

Another question on Engineering

question
Engineering, 04.07.2019 18:10
Steel is coated with a thin layer of ceramic to protect against corrosion. what do you expect to happen to the coating when the temperature of the steel is increased significantly? explain.
Answers: 1
question
Engineering, 04.07.2019 18:10
Coiled springs ought to be very strong and stiff. si3n4 is a strong, stiff material. would you select this material for a spring? explain.
Answers: 2
question
Engineering, 04.07.2019 18:10
Water at 55c flows across a flat plate whose surface temperature is held constant at 95c. if the temperature gradient at the plate's surface for a given value of x is 18 c/mm, find a) local heat transfer coefficient. b) heat flux
Answers: 3
question
Engineering, 04.07.2019 18:10
Carbon dioxide gas expands isotherm a turbine from 1 mpa, 500 k at 200 kpa. assuming the ideal gas model and neglecting the kinetic and potential energies, determine the change in entropy, heat transfer and work for each kilogram of co2.
Answers: 2
You know the right answer?
In an air-standard brayton cycle the air enters the compressor at 100 kpa and 10°c, with a mass flow...
Questions
question
Mathematics, 27.09.2020 15:01
question
Social Studies, 27.09.2020 15:01
question
Spanish, 27.09.2020 15:01
question
Geography, 27.09.2020 15:01
question
Chemistry, 27.09.2020 15:01
Questions on the website: 13722361