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Common data for 6, 7 & 8:
In adiabatic turbine, air enters at 550 kPa, 425K and leaves at 110kPa, 325K. The inlet and exit velocities of air are 150m/s and 50m/s respectively
T0 = 250C, CP = 1.005 kJ/kg-K, R = 0.287 kJ/kg-K
Q. Actual work will be:-
  • a)
    170.2 kJ/kg
  • b)
    210 kJ/kg
  • c)
    160 kJ/kg
  • d)
    110.5 kJ/kg
Correct answer is option 'D'. Can you explain this answer?
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Common data for 6, 7 & 8:In adiabatic turbine, air enters at 550 k...
Answer is (d)
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Common data for 6, 7 & 8:In adiabatic turbine, air enters at 550 k...
Steady flow energy equation is given for adiabatic nozzle neglecting P.E h1+((c1)^2)/2=h2+((c2)^2)/2+W h=Cp*T Give importance to equalising units in both enthalpy term as well as ke due to velocity term
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Common data for 6, 7 & 8:In adiabatic turbine, air enters at 550 k...
The common data for 6 and 7 is that they are both positive integers.
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Common data for 6, 7 & 8:In adiabatic turbine, air enters at 550 kPa, 425K and leaves at 110kPa, 325K. The inlet and exit velocities of air are 150m/s and 50m/s respectivelyT0 = 250C, CP = 1.005 kJ/kg-K, R = 0.287 kJ/kg-KQ. Actual work will be:-a)170.2 kJ/kgb)210 kJ/kgc)160 kJ/kgd)110.5 kJ/kgCorrect answer is option 'D'. Can you explain this answer?
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Common data for 6, 7 & 8:In adiabatic turbine, air enters at 550 kPa, 425K and leaves at 110kPa, 325K. The inlet and exit velocities of air are 150m/s and 50m/s respectivelyT0 = 250C, CP = 1.005 kJ/kg-K, R = 0.287 kJ/kg-KQ. Actual work will be:-a)170.2 kJ/kgb)210 kJ/kgc)160 kJ/kgd)110.5 kJ/kgCorrect answer is option 'D'. Can you explain this answer? for Mechanical Engineering 2024 is part of Mechanical Engineering preparation. The Question and answers have been prepared according to the Mechanical Engineering exam syllabus. Information about Common data for 6, 7 & 8:In adiabatic turbine, air enters at 550 kPa, 425K and leaves at 110kPa, 325K. The inlet and exit velocities of air are 150m/s and 50m/s respectivelyT0 = 250C, CP = 1.005 kJ/kg-K, R = 0.287 kJ/kg-KQ. Actual work will be:-a)170.2 kJ/kgb)210 kJ/kgc)160 kJ/kgd)110.5 kJ/kgCorrect answer is option 'D'. Can you explain this answer? covers all topics & solutions for Mechanical Engineering 2024 Exam. Find important definitions, questions, meanings, examples, exercises and tests below for Common data for 6, 7 & 8:In adiabatic turbine, air enters at 550 kPa, 425K and leaves at 110kPa, 325K. The inlet and exit velocities of air are 150m/s and 50m/s respectivelyT0 = 250C, CP = 1.005 kJ/kg-K, R = 0.287 kJ/kg-KQ. Actual work will be:-a)170.2 kJ/kgb)210 kJ/kgc)160 kJ/kgd)110.5 kJ/kgCorrect answer is option 'D'. Can you explain this answer?.
Solutions for Common data for 6, 7 & 8:In adiabatic turbine, air enters at 550 kPa, 425K and leaves at 110kPa, 325K. The inlet and exit velocities of air are 150m/s and 50m/s respectivelyT0 = 250C, CP = 1.005 kJ/kg-K, R = 0.287 kJ/kg-KQ. Actual work will be:-a)170.2 kJ/kgb)210 kJ/kgc)160 kJ/kgd)110.5 kJ/kgCorrect answer is option 'D'. Can you explain this answer? in English & in Hindi are available as part of our courses for Mechanical Engineering. Download more important topics, notes, lectures and mock test series for Mechanical Engineering Exam by signing up for free.
Here you can find the meaning of Common data for 6, 7 & 8:In adiabatic turbine, air enters at 550 kPa, 425K and leaves at 110kPa, 325K. The inlet and exit velocities of air are 150m/s and 50m/s respectivelyT0 = 250C, CP = 1.005 kJ/kg-K, R = 0.287 kJ/kg-KQ. Actual work will be:-a)170.2 kJ/kgb)210 kJ/kgc)160 kJ/kgd)110.5 kJ/kgCorrect answer is option 'D'. Can you explain this answer? defined & explained in the simplest way possible. Besides giving the explanation of Common data for 6, 7 & 8:In adiabatic turbine, air enters at 550 kPa, 425K and leaves at 110kPa, 325K. The inlet and exit velocities of air are 150m/s and 50m/s respectivelyT0 = 250C, CP = 1.005 kJ/kg-K, R = 0.287 kJ/kg-KQ. Actual work will be:-a)170.2 kJ/kgb)210 kJ/kgc)160 kJ/kgd)110.5 kJ/kgCorrect answer is option 'D'. Can you explain this answer?, a detailed solution for Common data for 6, 7 & 8:In adiabatic turbine, air enters at 550 kPa, 425K and leaves at 110kPa, 325K. The inlet and exit velocities of air are 150m/s and 50m/s respectivelyT0 = 250C, CP = 1.005 kJ/kg-K, R = 0.287 kJ/kg-KQ. Actual work will be:-a)170.2 kJ/kgb)210 kJ/kgc)160 kJ/kgd)110.5 kJ/kgCorrect answer is option 'D'. Can you explain this answer? has been provided alongside types of Common data for 6, 7 & 8:In adiabatic turbine, air enters at 550 kPa, 425K and leaves at 110kPa, 325K. The inlet and exit velocities of air are 150m/s and 50m/s respectivelyT0 = 250C, CP = 1.005 kJ/kg-K, R = 0.287 kJ/kg-KQ. Actual work will be:-a)170.2 kJ/kgb)210 kJ/kgc)160 kJ/kgd)110.5 kJ/kgCorrect answer is option 'D'. Can you explain this answer? theory, EduRev gives you an ample number of questions to practice Common data for 6, 7 & 8:In adiabatic turbine, air enters at 550 kPa, 425K and leaves at 110kPa, 325K. The inlet and exit velocities of air are 150m/s and 50m/s respectivelyT0 = 250C, CP = 1.005 kJ/kg-K, R = 0.287 kJ/kg-KQ. Actual work will be:-a)170.2 kJ/kgb)210 kJ/kgc)160 kJ/kgd)110.5 kJ/kgCorrect answer is option 'D'. Can you explain this answer? tests, examples and also practice Mechanical Engineering tests.
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