On the axis provide, draw a corresponding T-s diagram for the Brayton cycle shown giventhe following information:iv.V.vi.Compressor 1 is reversible, but Compressor 2 and the turbine are irreversible.The pressure drops through the regenerator are combustors are negligible.The pressures at state (1) and state (10) are equal to the atmospheric pressure.T8RegeneratorfmmmmmQinCombustorCompressorCompressorTurbineWcycleIntercoolermmCour

Answered: Image /qna-images/answer/37a5bc81-6ecb-466d-9f09-dc6e28b3a22a.jpg

Answered: On the axis provide, draw a…

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

Problem 1.1MA

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Ts diagrams for two reversible thermodynamic power cycles are shown in the following figure. Both cycles operate between a high temperature reservoir at 500 K and a low temperature reservoir at 300 K. The process on the left is the Carnot cycle described in Section 2.9. The process on the right is a Stirling cycle, which is similar to a Carnot cycle, except that the two steps (state 4 to state 1) and (state 2 to state 3) are at constant volume. Which cycle, if either, has a greater efficiency? Explain.
Write the expression for efficiency of a Rankine cycle in terms of Wturb, Wpump, Qin, Qout, and enthalpies. Thermodynamics question briefly explanation please
Ts diagrams for two reversible thermodynamic power cycles are shown in the following fig- ure. Both cycles operate between a high temperature reservoir at 500 K and a low temperature reservoir at 300 K. The process on the left is the Carnot cycle described in Section 2.9. The process on the right is a Brayton cycle, which is similar to a Carnot cycle, except that the two steps (state 1 to state 2) and (state 3 to state 4) are at constant pressure. Which cycle, if either, has a greater efficiency? Explain.
Derive the formula of efficiency of the following: b. Diesel Cycle in terms of cutoff ratio rc, specific heat ratio k and compression r
Get the following values for each stage: Stage 3: P3, T3, S3, H3 Stage 4: P4, T4, S4, H4 Explain how to get values please.
Rankine Cycle What two conditions can you define for state 2 (pump) that are inferred from other states?
This is a Diesel cycle Ideal gas model, constant specific heat R= 0.287 kj/kg-k Cv = 0.717 (kj/kg-k) Cp=1.004 [ kj/kg-k) gamma = 1.4 find entropy at each state s (kj/kg-k) at state 1 P1=200Kpa T1 =300K at state 2 P2=7000KPA T2=828.48K at state 3 P3=7000KPA T3=1500K at state 4 P4=459.16Kpa T4=688.74K Example @stATE 1 p1= 95 KPA t1 = 290K ANSWER : s1 = 1 kj/kg-k how it happen?
Can you please answer question 4
Please answer D and E thank you
Only answer part2.
In an air standard brayton cycle, air enters the compressor at 27 degree C and 100 kPa. The pressure ratio is 10, and the maximum allowable temperature is 1350 K. the compressor and turbine efficiencies are 85%, and pressure drops 27 kPa between the compressor discharge and turbine inlet. Determine the pressure and temperature at each state in the cycle, the compressor and turbine work, and the cycle thermal efficiency. Please show the PV and TS diagram. Please show complete formulas and solutions.
In the first stage of the impulse turbine, the adiabatic heat drop in the nozzle is 350 (kJ/kg), the velocity coefficient of the nozzle is 0.96, the nozzle exit angle is 20 degrees, the circumferential speed of the rotor is 350 m/s, the rotor The exit angle is 30 degrees. Find the next value.(1) Nozzle efficiency, (2) Draw a velocity triangle (scale), (3) Circumferential force acting on the rotor blade (4) Find the forward efficiency of the turbine.

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