Required informationProblem 05.051-Turbine flowSteam flows steadily through an adiabatic turbine. The inlet conditions of the steam are 4 MPa, 500°C, and 80 m/s and theexit conditions are 30 kPa, 92 percent quality, and 50 m/s. The mass flow rate of the steam is 11.80 kg/s. The properties ofthe steam areV₁ = 0.086442 m³/kg, h₁ = 3446 kJ/kg, and h₂P₁ =4 MPaT₁ = 500°CV₁ = 80 m/s3446 kJ/kg, and h₂ 2437. 7 kJ/kg.Steamm kg/sP₂= 30 kPax2=0.92V2= 50 m/sProblem 05.051.c - Turbine flowDetermine the turbine inlet area. (Round the final answer to three decimal places.)The turbine inlet area ism².

To determine the turbine inlet area, we can use the following relation derived from the continuity…

Answered: Required information Problem…

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

See similar textbooks

Similar questions

6) Steam enters a turbine at a pressure P-2.0MPA, temperature T1=500°C and enthalpy hi=3062 kJ/kg with a velocity Vi=10 m/s. The steam leaves the turbine as a gas-liquid mixture at a pressure P2=101kPa, temperature T2-373 K, and enthalpy ha=2621 kJ/kg with a velocity of v2-50 m/s. Thermal energy is lost through the turbine walls at a rate of 5 kJ/hr. The elevation difference between the entrance and exit of the turbine can be neglected. Calculate the power output in units of kW if 4000 kg/hr of steam pass through the turbine. %3D 4ニ-13815/5ec Pi thz + 6. 2Xla メSo? 2K9.81 3062 x103 1389 10 + é 621 X1s*) !8א2 ll rel 1o0ox4.21 looo X 9.81 2.
Air at a 800 kPa and 1300 K enters an adiabatic and reversible turbine with a mass ﬂow rate 6 kg/s. The outlet pressure is 100 kPa and assume that speciﬁc heats are constant and evaluated at 600 K. What is the specific heat at constant pressure for this problem? What is the temperature of the outlet in K? Round your answer to one decimal place. How much power is produced in kW? Round your answer to the nearest whole number.
P Steam turbine Wout P2 x2 = 1.0 V2 Steam enters a well-insulated turbine at 4.0 MPa and T1°C with a velocity of 100 m/s. At the exit, water is saturated vapor at 20 kPa and the velocity is 180 m/s. What should be inlet temperature T1, in °C, if work generated by turbine (wout) is 600 kJ/kg.
Please check attach file
1- Nitrogen is stored in a large chamber under conditions of 450 K and 1.5 x 105 N/m . The gas leaves the chamber through a convergent-only nozzle whose outlet area is 30 cm .The ambient room pressure is 1 × 105 N/m, and there are no losses. (a) What is the velocity of the nitrogen at the nozzle exit? (b) What is the mass flow rate? (c) What is the maximum flow rate that could be obtained by lowering the ambient pressure? ERING RINC
A blade pair in an axial flow compressor is being designed. The axial flow component of gas velocity is 174m/s. The engine diameter at the mean blade height is 0.73m and the blade height at the rotor inlet is 0.21m. The rotor's absolute inlet flow angle is 26 degrees. The stagnation conditions at the inlet to the blade pair are 298K and 130kN/m² Using Cp 1.005k/kg/K, R-0.287k/kg/K, and taking the ratio of specific heat capacities as 1.4, calculate the engine mass flow rate to the nearest kg/s
Thank you so much can you hand write clear please
Your second customer wants to determine the dissipated electrical power by a personal computer, which has a fan that draws 5 L/s of air at 101.325 kPa and 21°C through the box containing the CPU and other components. After that air leaves at 101.325 kPa and 30 °C. Part 1Derive the steady flow energy equation (SFEE) from the first principles. You are required to show all the steps in deriving the SFEE and using both the principles of mass and energy conversation.Part 2Produce specific steady state energy equation (SFEE) by stating all the stated assumption in this equipment in order to be used in later stages without further analysis. Then calculate the pump power.Part 3Apply the short form to determine the dissipated electrical power by the personal computer.
A gas flows steadily through a rotary compressor at a temperature of 16 ⁰C, a pressure of 100kPa, and an enthalpy of 392.2 kJkg-1. The gas leaves the compressor at a temperature of 245⁰C, a pressure of 0.6 MPa and an enthalpy of 534.5 kJkg-1. There is no heat transfer to or fromthe gas as it flows through the compressor. Using the steady flow equation appropriate toeach case, evaluate the external work done per unit mass of gas: a) when the inlet and exit velocities of the gas are negligible b) when the inlet velocity of the gas is 80 ms-1 and the exit velocity of the gas is 160 ms-1.
Carbon dioxide (??=28.2 J/mol⋅K)(Cp=28.2 J/mol⋅K) enters a steady‑state adiabatic compressor at 100.0 kPa100.0 kPa and 320.10 K320.10 K and exits at 1000.0 kPa1000.0 kPa and 573.0 K.573.0 K. What is the entropy of generation (kJ/kmol⋅K)? Is it feasible?
A turbine operates under steady flow conditions, receiving steam at the following state: pressure 1200kPa, temperature 188℃, enthalpy 2785 KJ/kg, speed=33.3m/s and elevation of 3m . The steam leaves the turbine at the following state; pressure=20kPa, enthalpy 2512 kJ/kg. Speed 100m/s and elevation 0 m. Heat is lost to the surroundings at the rate of 0.29 kJ/s. If the rate of steam flow through a turbine is 0.42 kg/s, what is the power output of the turbine in kW?
Required information Problem 05.051-Turbine flow Steam flows steadily through an adiabatic turbine. The inlet conditions of the steam are 4 MPa, 500°C, and 80 m/s and the exit conditions are 30 kPa, 92 percent quality, and 50 m/s. The mass flow rate of the steam is 11.80 kg/s. The properties of the steam are V₁ = 0.086442 m³/kg, h₁ 3446 kJ/kg, and h₂ 2437.7 kJ/kg. P=4 MPa T₁ = 500°C V₁ = 80 m/s Steam mkg/s P₂= 30 kPa *2=0.92 V2= 50 m/s Problem 05.051.a - Turbine flow Determine the change in kinetic energy. The change in kinetic energy is kJ/kg.

SEE MORE QUESTIONS

Recommended textbooks for you

Elements Of Electromagnetics

Mechanical Engineering

ISBN:

9780190698614

Author:

Sadiku, Matthew N. O.

Publisher:

Oxford University Press

Mechanics of Materials (10th Edition)

Mechanical Engineering

ISBN:

9780134319650

Author:

Russell C. Hibbeler

Publisher:

PEARSON

Thermodynamics: An Engineering Approach

Mechanical Engineering

ISBN:

9781259822674

Author:

Yunus A. Cengel Dr., Michael A. Boles

Publisher:

McGraw-Hill Education

Elements Of Electromagnetics

Mechanical Engineering

ISBN:

9780190698614

Author:

Sadiku, Matthew N. O.

Publisher:

Oxford University Press

Mechanics of Materials (10th Edition)

Mechanical Engineering

ISBN:

9780134319650

Author:

Russell C. Hibbeler

Publisher:

PEARSON

Thermodynamics: An Engineering Approach

Mechanical Engineering

ISBN:

9781259822674

Author:

Yunus A. Cengel Dr., Michael A. Boles

Publisher:

McGraw-Hill Education

Control Systems Engineering

Mechanical Engineering

ISBN:

9781118170519

Author:

Norman S. Nise

Publisher:

WILEY

Mechanics of Materials (MindTap Course List)

Mechanical Engineering

ISBN:

9781337093347

Author:

Barry J. Goodno, James M. Gere

Publisher:

Cengage Learning

Engineering Mechanics: Statics

Mechanical Engineering

ISBN:

9781118807330

Author:

James L. Meriam, L. G. Kraige, J. N. Bolton

Publisher:

WILEY

SEE MORE TEXTBOOKS