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help please!! please write clearly and in detail ! this is one questions with multiple questions...
please help! write crealy and i. detail thisnis one problem usign this information Question 14 (6 points) Q4. For this part of the problem, use the same main problem statement, numbers, and image in Q4 (1). (3) Determine the volume flow rate (in m3/s) of the steam at the nozzle exit. Your answer must include 3 places after the decimal point. Question 12 (6 points) Q4. Steam enters a nozzle at 332°C and 600 kPa with a velocity of 11...
please help! write clearly and in detail . this is one problem divided into three questions . the numbers used would be from the last pic Question 10 (10 points) Q3. For this part of the problem, use the same main problem statement, numbers, and image in Q3 (1). (2) Determine the overall boundary work (in kJ) involved in this entire process. Negative sign must be included if the work is done to the system. Your answer must include 1...
THERMO: QUESTION 5 Saturated water vapor at 12.92 bar enters an insulated throttling valve which drops the pressure to 1.50 bar. Determine the temperature (oC) of the steam at the exit of the valve. Note: Give your answer to two decimal places. QUESTION 6 Air enters an adiabatic diffuser at 320 K and 100 kPa with a velocity of 665.4 m/s. At the diffuser exit, the temperature is 520 K. Determine the velocity (m/s) at the exit of the diffuser....
Need help with problem 5.26, help me understand, please explain in detail and write clearly. thanks in advance. 5.24 Water enters the horizontal, circular cross-sectional, sudden- contraction nozzle sketched in Fig. P5.24 at section (1) with a uniformly distributed velocity of 7.5 m/s and a pressure of 500 kPa. The water exits from the nozzle into the atmosphere at section (2) where the uniformly distributed velocity is 30 m/s. Determine the axial component of the anchoring force required to hold...
Homework Problem IW8 3 Attemps Used 20 Due DateThu, Jul 30, 2020, 23:59:59 Current Time Thu, Jul 30, 2020, 00:02:48 Air flows through a converging-diverging nozzle/differ. Assuming isentropic flow, air as an ideal gas, and constant specific heat determine the state at several locations in the system Note: The specific heat ratio and gas constant for air are given ask-1A od R-0.287 kg K respectively --Given Vues Inlet Temperature: TI (K) 358 Inlet pressure: PI (kPa) - 626 Inlet Velocity:...
PLEASE answer all questions clearly Problem 6.109 SI As shown in the figure below, air enters the diffuser of a jet engine at 18 kPa, Ti 250 K with a velocity of V1 = 201 m/s, all data corresponding to high-altitude flight. The air flows adiabatically through the diffuser, decelerating to a velocity of 50 m/s at the diffuser exit. DiffuserCompressor Combustors Giurbine -Nozzle P1-18 kPa Ti,V V2-50 m/s Air Product in gases out Assume steady-state operation, the ideal gas...
UBAV Air flows through a converging-diverging nozzle diffuser. A normal shock stands in the diverging section of the nozzle. Assuming isentropie flow, air as an ideal gas, and constant specific heat determine the state at several locations in the system. Solve wsing equations rather than with the tables Note: The Specific heat ratio and gas constant for air are given as k-1 and R 0.287 kJ/kg-K respectively Give Values Inlet Temperature: TI(K)-340 Inlet pressure: P1 (kPa) - 550 Inlet Velocity:...
need help with letter j,k,l,m,n,o just those i solved the top ones just the last 6 thanjs you mine the temperature (K) at the throat. Your Answer=289.711 Correct! Exact Answer=289.71 +/- 1.0E+00 e) Determine the velocity (m/s) at the throat. Your Answer 341.18 Correct! Exact Answer 341.183 +/- 1.3E+00 f) Determine the pressure (kPa) at the throat. Your Answer=314.09 Correct! Exact Answer=314.10 +/- 1.2E+00 g) Determine the mass flow rate (kg/s) through the nozzle Your Answer=1.0826 Correct! Exact Answer= 1.08264...
Homework Problem HW8 2 Attemps Used 2/20 Due Date - Thu, Jul 30, 2020, 23:59:59 Current Time Thu, Jul 30, 2020, 01:42:09 Air flows through a converging-diverging nozzle/diffuser. A normal shock stands in the diverging section of the nozzle. Assuming sentropic flow, air as an ideal gas, and constant specific heats determine the state at several locations in the system. Solve using equations rather than with the tables Note: The specific heat ratio and gas constant for air are given...
Can some one solve this question please Q4) A steam turbine at steady state is operated at part load by throttling the steam to a lower pressure before it enters the turbine. Before throttling, the pressure and temperature are, respectively, 1.5 MPa and 320°C. After throttling, the pressure is 1 MPa. At the turbine exit, the steam is at 8 kPa and a quality of 90%. Heat transfer with the surroundings and all kinetic and potential energy effects can be...