Air enters an adiabatic nozzle at 400 kpa. The inlet area of the nozzle is 110 cm2.

Air enters an adiabatic nozzle at 400 kpa 4. Air enters an adiabatic nozzle steadily at 300 kPa, 200°C, and 30 m/s and leaves at 100 kPa and 180 m/s. If the air undergoes an adiabatic expansion process through the nozzle, what is the maximum velocity of the air at the nozzle exit in m/s? Use the table containing the ideal gas specific heats of various common gases. If the isentropic efficiency of the nozzle is 90 percent, determine the exit temperature and Question: Air enters an adiabatic nozzle steadily at 400 kPa, 250°C, and 40 m/s and leaves at 200 kPa and 200 m/s. Air enters an adiabatic nozzlę at 500 kPa and 400 K with a velocity of 50 m/s and exits at 400 kPa and 365 K. Determine (a) the exit temperture, and (b) the exit pressure of the air. The mass flow rate is 2 kg/s and the inlet area is 1 m^2. We need to determine the exit pressure and temperature. 005 kJ/kg K, %3D Transcribed Image Text: 5-36 Air enters an adiabatic nozzle steadily at 300 kPa, 200°C, and 45 m/s and leaves at 100 kPa and 180 m/s. (Use: T0= 20°C) Question: Air at 500 kPa and 400 K enters an adiabatic nozzle at a velocity of 30 m/s and leaves at 300 kPa and 350 K. Determine (a) the mass flow rate through Air enters an adiabatic nozzle steadily at 300 kPa, 200°C, and 30 m/s and leaves at 100 kPa and 180 m/s. To determine the isentropic efficiency (η), we can compare the actual change in specific enthalpy (h) to the ideal change in specific enthalpy. Engineering; Question. Using variable specific heats, determine (a) the isentropic efficiency (b) the exit velocity (c) Air enters an air compressor operating at a steady state with a volumetric flow rate of 37 m 3 per minute at 136 kPa and 305 K. Air enters an adiabatic nozzle at 400 k P a 400 \mathrm{~kPa} 400 kPa and 54 7 ∘ C 547^{\circ} \mathrm{C} 54 7 ∘ C with low velocity and exits at 240 m / s 240 \mathrm{~m} / \mathrm{s} 240 m / s. Air's entropy change for this process Question: !Required informationProblem 08. Determine the exit temperature. The heat loss from the nozzle to the Air enters an adiabatic nozzel steadily at 400 kPa, 250 oC, and 40 m/s and leaves and 70 m/s. If the isentropic effi- ciency of the nozzle is 90 percent, determine the exit tempera- ture and pressure of the air. 005 m 2 is fitted to the wall of the reservoir as shown in the figure. STEAM 2- Air at 80 kPa, 27°C, and 220 m/s enters a diffuser at a rate of 2. To Find: The exit pressure and exit temperature. Answered step-by-step. Determine the Question: Q. at 250 kPa P 400 kPa T-250 C 40 m/sAIR250 kPa A) Determine the mass flow rate through the nozzle (kg/'s). 8 MPa and 400°C. Result: (a) The isentropic efficiency is 0. Using variable specific heats determine a) The isentropic efficiency b) The exit velocity; Air at 600 kPa and 500 K enters an adiabatic nozzle that has an inlet to exit area ratio of 2:1 with a velocity of 380 m/s. 2k points) Air enters an adiabatic nozzle steadily at 300 kPa, 200°C, and 30 m/s and leaves at 100 kPa and 180 m/s. 6 MPa and 250°C at a rate of 0. (b) the isentropic efficiency, and (c) the entropy generation. (Upload detailed working for partial credits) O A. Using variable specific heats, determine (a) the isentropic efficiency, (b) the exit velocity, and (c) the entropy generation. Calcula; Steam enters a nozzle at 400 ? C and 800 kPa with a velocity of 10 m/s, and leaves at 300 ? C and 200 kPa while losing heat at a rate of 25 kW The air mass flow rate is 25 kg/s. The inlet area of the nozzle is 80 cm 2. Calculate the mass flow rate of air and the required power input. The enthalpy of air at the inlet temperature of 500 K is h1 = 503. 5 kg/s and leaves at 42°C. Air enters an adiabatic nozzle at 300 kPa, 200 C, and 30 m/s. Use the table containing the ideal gas properties of air. Suggestion for further study: Reconsider problem (1). Assuming air to be an ideal gas with variable specific heats and disregarding any irreversibilities , determine the exist velocity of the air Steam enters an adiabatic nozzle at 400^\circ and 800 kPa with a velocity v = 50 m/s, it leaves the nozzle at 300^\circ and 200 kPa. 0204 kJ/kgK O B. Here’s the best way to solve it. A converging diverging nozzle of exit area 0. asked Feb 26, 2022 in General by Niralisolanki (115k points) closed Feb 28, 2022 by Niralisolanki. Air enters an adiabatic nozzle steadily at 300 kPa, 200 ∘ ^\circ{} ∘ C, and 45 m/s and leaves at 100 kPa and 180 m/s. Question: Air at 400 kPa and 400 K enters an adiabatic nozzle at a velocity of 40 m/s and leaves at 250 kPa and 360 K. At the nozzle exit, the air is at 70 kPa, 450°C. Problem 08. Determine the isentropic efficiency. Determine (a) The isentropic efficiency (b) The exit velocity (c) The entropy generat; Air enters an adiabatic turbine steadily at 1600 kPa and 450 degrees C with a velocity of 55. (b) The exit velocity is 30 m/s. Answers: (a) 437 K, (b) 331 kPa. The air at 500 kPa and 400 K enters an adiabatic nozzle at a velocity of 30 m/s and leaves at 300 kPa and 350 K. Determine a. Solution . In an adiabatic nozzle, the process is assumed to be reversible and adiabatic, meaning there is no heat transfer and the entropy remains constant. Determine (a) the mass flow rate through the nozzle, (b) the exit temperature Air enters an adiabatic nozzle at 400 kPa and 900 K with negligible velocity. The inlet area of the nozzle is 1 Question: 7-119 Air enters an adiabatic nozzle at 400 kPa and 547°C with low velocity and exits at 240 m/s. °C. 7 K. leaves at 100 kPa. Question: Air at 500kpa and 400K enters an adiabatic nozzle at a velocity of 30m/s and leaves at 300 kpa and 350k, using variable specific heats, determine a: the isentropic efficiency, b:the exit velocity and c the entropy generation Question: Air at 500kPa and 400K enters an adiabatic nozzle at a velocity of 35m/s and leaves at 300kPa and 350K. Using variable specific heals, determine (a) the isentropic efficiency. --- Show Question: Air (ideal gas) enters an adiabatic nozzle steadily at 200 kPa, 600°C,and 60 m/s and leave at 70 kPa and 400 °C. 85 ^oC, and a velocity of 40 m/s. Determine Air enters an adiabatic nozzle steadily at 400 kPa, 200°C, and 40 m/s and leaves at 120 kPa and 210 m/s. Theinitial state is 1400 kPa and 815 degsC and the final pressure is140 kPa. (b) The exit velocity. Literature guides Concept explainers Writing guide Popular textbooks Popular high school textbooks Popular Q&A The air at 500 kPa and 400 K enters an adiabatic nozzle at a velocity of 30 m/s and leaves at 300 kPa and 350 K. If the air undergoes an adiabatic expansion process through the nozzle, what is the maximum velocity of the air at the nozzle exit in m / s \mathrm{m} / \mathrm{s} m / s? Q2/ Air enters an adiabatic nozzle steadily at 400 kPa, 290°C, and 35 m/s and leaves at 200 kPa and 240 m/s. 5-36. The air is to exit at 100 kPa with velocity of Air enters an adiabatic nozzle steadily at 300 kPa, 200 ∘ ^\circ{} ∘ C, and 45 m/s and leaves at 100 kPa and 180 m/s. Air enters an adiabatic diffuser at 320 K and 100 kPa with a velocity of 643. Isentropic efficiency of the nozzle 3. 2022 India Languages Secondary School answered Air enters an adiabatic nozzle at 300 KPa, 500K with a velocity of 10 m/s It leaves the nozzle at 100 KPa with a Air at 5 0 0 kPa and 4 0 0 K enters an adiabatic nozzle at a velocity of 3 0 m s and leaves at 3 0 0 kPa and Using variable specific heats, determine ( a ) the isentropic efficiency, ( b ) the exit velocity, and ( c ) the entropy generated per k g of air flowing through the nozzle associated with this Air at 500 kPa and 400 K enters an adiabatic nozzle at a velocity of 30 m/s and leaves at 300 kPa and 350 K. The air pressure increases from 50 kPa to 800 kPa while heat is removed from The correct answer is 3) a) 0. 0 m/s and leaves at 150 kPa with a velocity if 150 m Question: Air enters an adiabatic nozzle at 400 kPa, 277 °C, and 60 m/s and exits at 80 kPa. Using variable specific heats, determine (a) The isentropic efficiency, (b) The exit velocity, and (c) The entropy generation. The specific heat of air C P, is 1008 J/kg. Chapter 7 problem Air at 500 kPa and 400 K enters an adiabatic nozzle at a velocity of 30 m/s and leaves at 300 kPa and 350 K. In a gas turbine installation air is heated inside heat exchanger upto 750C from ambient temperature of 27C Hot air then enters into gas turbine with the velocity of 50 m/s and leaves at 600C Air leaving turbine enters a nozzle at 60 m/s velocity and leaves nozzle at temperature of 500C For unit mass flow rate of air determine the following assuming adiabatic 5-36 Air enters an adiabatic nozzle steadily at 300 kPa, 20 0 ∘ C, and 45 m / s and leaves at 100 kPa and 180 m / s. b) eta_N = Round to three decimal places. 92 kJ/kg, v 2 = 0. The inlet of the nozzle is 90 cm^2 It exits at 200 kPa and a velocity of 151. Determine (a) The isentropic efficiency (b) The exit velocity (c) The entropy generat; Air enters a compressor at a steady volume flow rate of 50 m ^3/min. The air is accelerated from 10 m/s to 200 m/s by the nozzle. The inlet area of the nozzle is 75 cm2. Determine (a) the mass flow rate through the nozzle, (b) the exit temperature of the air and (c) the exit area of the nozzle. Find (a) the exit temperature of the air and (b) the exit area of the diffuser 14 MPa and 60°C The compressors The R-134a enters an adiabatic Air enters an adiabatic nozzle at 500 kPa, 650^{\circ}C. Determine the exit temperature and pressure of the air. Exergy destruction per Air is expanded in an adiabatic nozzle during a polytropic process with n = 1. Science. Determine (a) The isentropic efficiency (b) The exit velocity (c) The entropy generat; Air enters a well-insulated nozzle with a pressure of 1100 kPa, a temperature of 626. 084-m² opening. The inlet area is 80 cm2. The velocity of the air at the entry is 100 m/s, and at the exit, it is 360 m/s. 0102 kJ/kgK D. 6°C, (c) 38. if the isentropic efficiency of the nozzle is 90 percent. Using variable specific heats, determine (a ) the isentropic efficiency, (b) the exit velocity, and (c) the entropy generation. Exit velocity of the air (m/s) b. 11. engineering. = Air P1 = 300 kPa T1 = 200°C Vi = 45 m/s Aj = 110 cm P2 = 100 Air at 200 kPa and 950 K enters an adiabatic nozzle at low velocity and is discharged at a pressure of 80 kPa. Find step-by-step Engineering solutions and the answer to the textbook question Air at 500 kPa and 400 K enters an adiabatic nozzle at a velocity of 30 m / s and leaves at $300 kPa$ and $350 K$. Using EES software, investigate the Air enters an adiabatic steady flow nozzle at 470 kPa and 52 7 ∘ C with low velocity and exits at 260 m / s. It enters the nozzle at 700 kPa and 100 degrees C with a velocity of 30 m/s and exits at a pressure of 200 kPa. The inlet area of the nozzle is 80 cm? Skip to main content. The exit velocity c. K (Table A-1). 319 b) 0. Determine (a) The isentropic efficiency (b) The exit velocity (c) The entropy generat; Consider an adiabatic nozzle with air entering at 300 k and 450 kpa and a velocity of 20 m/s. Solution For Air at 500kPa and 400K enters an adiabatic nozzle at a World's only instant tutoring platform. Answers: 4. Using variable specific heats, determine the following: (a) The isentropic efficiency. Grade; Air enters an adiabatic nozzle at 400 kPa and 900 K with negligib | Air enters an adiabatic nozzle at 400 kPa and 900 K with negligible velocity. 3. The exit temperature b. 5605832 What is the rate of entropy generation for this turbine? . Air enters an adiabatic nozzle steadily at 300 kPa, 200 ∘ ^{\circ} ∘ C, and 45 m/s and leaves at VIDEO ANSWER: Air at 900 \mathrm{kPa} and 400 \mathrm{K} enters a converging nozzle with a negligible velocity. 8°C, and (c) 71 cm2) Air Air at 500 kPa and 400 K enters an adiabatic nozzle ai a velocity of 30 m/s and leaves at 300 kPa and 350 K. Using appropriate Steam enters a nozzle at 400 degree C and 800 kPa with a velocity of 10 m / s, and leaves at 375 degree C and 400 kPa while losing heat at a rate of 25 kW. Using variable specific heats determine a) The isentropic efficiency b) The exit velocity; Air at 80 kPa and 127 o C enters and adiabatic nozzle steadily at a rate of 1. Determine (a) the mass flow rate through the nozzle, (b) the exit temperature Solution for Q2/ Air enters an adiabatic nozzle steadily at 400 kPa, 290°C, and 35 m/s and leaves at 200 kPa and 240 m/s. Air enters the compressor through a 0. 012 kJ/kg⋅K. The dead state can be considered to be 100 kPa, 20°C. Create an engineering model with at least three (3) assumptions Determine: (a) The mass flow rate through the nozzle, (b) The exit temperature of the air, and (c) The exit area of the nozzle Cpr W Air at 800 kPa and 400?C enters a steady-flow nozzle with a low velocity and. The throat area of the nozzle is 10 \mathrm{cm}^{2} . 47 kg/s, (b) 231. 287 kJ/kgK) ln 500 kPa 300 kPa Δ s = − 0. Air at 500 kPa and 400 K enters an adiabatic nozzle that has an inlet-to-exit area ratio of 3:1 with a velocity of 100 m's and leaves with a velocity of 400 m/s. 532 K 3. The inlet area of the nozzle is 100 cm?. 287 kPa⋅m3/kg. The inlet area of nozzle is 60 cm2. State what the problem asks for and 5-39 Air enters an adiabatic nozzle steadily at 300 kPa, 200°C, and 45 m/s and leaves at 100 kPa and 180 m/s. The air is to exit at 100 kPa with velocity of 180 m/s Question: Air at 560 kPa and 500 K enters an adiabatic nozzle that has an inlet-to-exit area ratio of 2:1 with a velocity of 120 m/s and leaves with a velocity of 380 m/s. Using variable specific heats, determine (a) The isentropic efficiency, (b) The exit Using variable specific heats, Air at 80 kPa and 127°C enters an adiabatic diffuser steadily at a rate of 6000 kg/h and leaves at 100 kPa. Determine: Air as an Ideal-Gas: Properties The gas constant of air is 0. Using variable specific heats, determine (a) the isentropic efficiency, (b) the exit velocity, and (c) the entropy generation Air 500 kPa 400 K 30 m/s 300 kPa 350 K . 100 % (1 rating) Air at 500 kPa and 400 K enters an adiabatic nozzle at a velocity of 30 m/s and leaves at 300 kPa and 375 K. Steam enters an adiabatic nozzle at 3 MPa and 450°C with a velocity of 50 m/s and exits at 0. Repeat A converging nozzle has a throat area of 6 cm 2 and stagnation air condition of 120 kPa and 400 K. 287 kJ/kg K, Cp = 1. 17-90 Air flowing at 32 kPa, 240 K, and Mal — 3. 5 m 2. Find step-by-step Engineering solutions and the answer to the textbook question Air at 500 kPa and 400 K enters an adiabatic nozzle at a velocity of 30 m/s and leaves at 300 kPa and 350 K. Determine (1) The mass flow rate Air enters an adiabatic nozzle steadily at 400 kPa, 200oC, 35m/s and leaves at 150 kPa, 180 m/s. Step 1. 516 K 2. 0 votes . Determine The exit temperature and pressure of the air. Find step-by-step Physics solutions and your answer to the following textbook question: Air at 600 kPa and 500 K enters an adiabatic nozzle that has an inlet-to-exit area ratio of 2:1 with a velocity of 120 m/s and leaves with a velocity of Question: (6 points) Air at 570 kPa and 400 K enters an adiabatic nozzle at a negligible velocity and leaves at 160 kPa and 350 K. 429. Determine (a) The exit Find step-by-step Engineering solutions and the answer to the textbook question Air at 800 kPa and 400 degrees C enters a steady-flow nozzle with a low velocity and leaves at $100 \mathrm{kPa}$. The mass flow rate of air is 10 kg/s Question: 5–34 Air at 80 kPa and 127°C enters an adiabatic diffuser steadily at a rate of 6000 kg/h and leaves at 100 kPa. 0k views. 6 is forced to undergo an expansion turn of 150. a) V_2 = m/s Round to one decimal place. 67 kg/s and leaves at P = 60 kPa. Using variable specific heats, determine (a) the exit velocity in m/s and (b) the isentropic efficiency of the nozzle in %. Steam enters a nozzle at $400^{\circ} \mathrm{C}$ 06:25 Question. What is the isentropic efficiency of the nozzle? % What is the (actual) exit velocity of the air? sm What is the rate of Air at 500 kPa and 400 K enters an adiabatic nozzle at a velocity of 30 m/s and leaves at 300 kPa and 350 K. Using variable specific heats determine a) The isentropic efficiency b) The exit velocity; Air is compressed by an adiabatic compressor from 100 kPa and 12 C to a pressure of 800 kPa at a steady rate of 0. 2. The velocity of the airstream is decreased from 230 to 30 m/s as it passes through the diffuser. Do this problem TWO ways: 1) Assuming air is a thermally and calorically perfect gas with a ratio of specific heats, = Question: air enters an adiabatic frictionless nozzle at 400 K and 800 kPa, with a velocity of 4 m/s. If the isentropic 1- Air at 600 kPa and 500 K enters an adiabatic nozzle that has an inlet- to-exit area ratio of 2:1 with a velocity of 120 m/s and leaves with a velocity of 380 m/s. The inlet area is 80 cm 2. (a) What is the velocity at the nozzle exit? (b) What will happen to the exit velocity if there was heat loss during the expansion? (c) If the inlet and outlet difference in elevation was 3 m how much the velocity would be affected as Air at 500 kPa and 400 K enters an adiabatic nozzle at a velocity of 30 m/s and leaves at 300 kPa and 350 K. There are 2 steps to solve this one. 09 kJ/kg. The inlet area of the nozzle is 110 cm^2. Determine the entropy generation per unit mass. 0. Air flow of 2. The inlet area of the nozzle is 100 cm2. w Air enters an adiabatic nozzle steadily at 400 kPa, 300°C, and 30 m/s and leaves at 100 kPa and 200 m/s. Search Instant (0. Assuming that the expansion through the nozzle occurs ; Air enters an adiabatic nozzle at 45 psia and 940 F with low velocity and exits at 650 ft/s. The air exits at 50 kPa. The exit temperature is K. The velocity increases from 30m/s Q2/ Air enters an adiabatic nozzle steadily at 400 kPa, 290°C, and 35 m/s and leaves at 200 kPa and 240 m/s. What is the isentropic efficiency of the nozzle? % What is the actual) exit velocity of the air? m S What is the rate of entropy generation for this turbine? kJ kg K . The inlet area of nozzle is 110 cm{eq}^2{/eq}. 073 - Air entering and leaving an adiabatic nozzleAir at 500 kPa and 400 K enters an adiabatic nozzle at a velocity of \( 45. If the air undergoes an adiabatic expansion process through the nozzle, what is the maximum velocity of the air at the nozzle exit in m/s? Air enters an adiabatic nozzle steadily at 300 kPa, 200 ∘ ^\circ{} ∘ C, and 45 m/s and leaves at 100 kPa and 180 m/s. If the air undergoes an adiabatic expansion process through the nozzle, what is the maximum velocity of the air at the nozzle exit in m/s? Air enters an adiabatic nozzle at 45 psia and 940 F with low velocity and exits at 650 ft/s. write. Solution: This is a steady flow process since there is no change with time. If the isentropic efficiency of the nozzle is 92 percent, determine (a) the maximum possible exit velocity, (b) the exit temperature, and (c) the actual exit velocity of the air. 44 kPa . Determine: a) The mass flow rate through the nozzle, b) The exit temperature of the air, and c) The exit area of the nozzle. Note: Give your answer to two decimal places. If the flow is ideal and the exit pressure is 100 kPa, then . 83 kg/s enters a diffuser at 300 K Air at 800 kPa and 400°C enters a steady-flow nozzle with a low velocity and leaves at 100 kPa. Assume the flow is isentropic. the exit pressure of the nozzle is 100 kPa (near atmospheric pressure) and the exit temperature is 300 K (near room temperature). At the diffuser exit, the temperature is 520 K. Literature guides Concept explainers Writing guide Popular textbooks Popular high school textbooks Popular Q&A 5-35 Air at 600 kPa and 500 K enters an adiabatic nozzle that has an inlet-to-exit area ratio of 2:1 with a velocity of STEAM P₁ = 3 MPa T₁ = 400°C V₁ = 40 m/s P₂ = 2. Solution for Air at 500 kPa and 400 K enters an adiabatic nozzle at a velocity of 30 m/s and leaves at 300 kPa and 350 K. Show transcribed image text. (Answer: 0. Determine the following nformation: a. If the isentropic efficiency of the nozzle is 92% , determine the exits temperature and pressure of the air. . Determine (a) The isentropic efficiency (b) The exit velocity (c) The entropy generat; Air undergoes a steady-flow, reversible, adiabatic process. P1 = 300 kPa T1 = 200°C Vi = 45 m/s 11 - 110 cm Q. The Air enters an adiabatic nozzle at 400 k P a 400 \mathrm{~kPa} 400 kPa and 54 7 ∘ C 547^{\circ} \mathrm{C} 54 7 ∘ C with low velocity and exits at 240 m / s 240 \mathrm{~m} / \mathrm{s} 240 m / s. c) s_gen = kJ/kg middot K Question: <p>Air enters an adiabatic nozzle steadily at 300 kPa, 200&#176;C, and 30 m/s and<br />leaves at 100 kPa and 180 m/s. 2k points) thermodynamics Find an answer to your question Air enters an adiabatic nozzle at 300 KPa, 500K with a velocity of 10 m/s It leaves the nozzle at 100 KPa with a velocity of 180 aliasingh2131 aliasingh2131 03. The specific heat of air at the anticipated average temperature of 450 K is Cp=1. What is the velocity at the exit of the nozzle? Assume the specific heat is constant and can be taken at the average temperature between the inlet and outlet. The exit temperature is 341. Find step-by-step Engineering solutions and your answer to the following textbook question: Air enters an adiabatic nozzle steadily at $300 \mathrm{~kPa}$, $200^{\circ} \mathrm{C}$, and $30 \mathrm{~m} / \mathrm{s}$ and leaves at $100 \mathrm{~kPa}$ and $180 \mathrm{~m} / \mathrm{s}$. Determine: a) The exit temperature, Steam enters an adiabatic turbine at 8 MPa and 500 degrees Celsius with a mass flow rate of 3 kg/s and leaves at 30 kPa. the nozzle, what is the maximum velocity of the air at the nozzle exit, in m/s? Approximate answer: 800 m/s. Question: Air at 600 kPa and 500 K enters an adiabatic nozzle that has an inlet-to-exit area ratio of 2:1, with a velocity of 120 m/s and leaves with a velocity of 380 m/s. the mass flow rate of air through the nozzle B. ← Prev Question Next Question →. 100 % (3 Air at 800 kPa and 400°C enters a steady-flow nozzle with a low velocity and leaves at 120 kPa. Solution. Calculate the following: A. R = 0. Air is compressed by an adiabatic compressor from 100 kPa and 20°C to 1. 468 Air at 500 kPa and 400 K enters an adiabatic nozzle at a velocity of 30 m/s and leaves at 300 kPa and 350 K. The inlet Question: Air at 560kPa and 390 K enters an adiabatic nozzle at a negligible velocity and leaves at 110kPa and 350 K. The inlet conditions of the steam are 4. The diffuser and nozzle processes are; Air enters an adiabatic gas turbine at 1310 kPa and 400 degrees C and exits the turbine at 100 kPa and 125 degrees C. If the nozzle has an inlet area of 7. Determine (a) the mass flow rate through the nozzle, (b) the exit temperature In an adiabatic nozzle, the process is assumed to be reversible and adiabatic, meaning there is no heat transfer and the entropy remains constant. The maximum velocity of the air Air enters an adiabatic nozzle at 500 kPa and a temperature of 200 o C with a velocity of 100 m/s. Find step-by-step Engineering solutions and your answer to the following textbook question: Air at 600 kPa and 500 K enters an adiabatic nozzle that has an inlet-to-exit area ratio of 2:1 with a velocity of 120 m/s and leaves with a velocity of 380 m/s. Determine (a) the exit temperature and (b) the exit pressure of the air 2. 4 kg/s. Air at $600 \mathrm{kPa}$ and $500 \mathrm{K}$ enters an Air enters an adiabatic nozzle at 230 kPa, 600°C with a velocity of 60 m/s as shown in Figure P3. The gas constant of air is 0. a Air at 500 kPa and 400 K enters an adiabatic nozzle at a velocity of 30 m/s and leaves at 300 kPa and 350 K. 2 kg/s. a - Exit velocity of airDetermine the exit Solution for Air enters an adiabatic nozzle steadily at 300 Kpa, 200 °C and 30 m's then leaves at 100 Kpa and 180 m/s. 5 m², determine (a) the exit temperature and (b) the rate of entropy generation for this process. P1 300 kPa Tl-200°C Vi = 45 m/s A 110 cm2 P2 100 kPa v 1- Air at 600 kPa and 500 K enters an adiabatic nozzle that has an inlet-to-exit area ratio of 2:1 with a velocity of 120 m/s and leaves with a velocity of 380 m/s. Air flows steadily through an adiabatic turbine, entering at 1 MPa, 800 K, and 100 m/s and Air at 500 kPa and 400 K enters an adiabatic nozzle at a velocity of 100 m/s and leaves at 250 kPa and 350 K. The air exits at 200 kpa and 250 k. What is the isentropic efficiency of the nozzle? %What is the (actual) exit velocity of the air? msWhat is the rate of Thermodynamics 1. Find (a) the exit temperature of the air and (b) the exit area of the diffuser. Subjects Literature guides Concept explainers Writing guides Popular textbooks Popular high school textbooks Popular Air at 500 kPa and 400 K enters an adiabatic nozzle at a velocity of 50 m/s and leaves at 300 kPa and 350 K. (c) The entropy generation. It exits through a 0. The area of the inlet is 0. 828 What is the (actual) exit velocity of the air? 245. The isentropic efficiency Steam enters a nozzle at 400 degree C and 800 kPa with a velocity of 10 m / s, and leaves at 375 degree C and 400 kPa while losing heat at a rate of 25 kW. 043358 m 3 /kg, h 1 = 358. Find the entropy generation. Using variable specific heats, Homework Help is Here – Start Your Trial Now! learn. Using variable specific heats, Determine the following A. Air at 500 kPa and 400 K enters an adiabatic nozzle at a velocity of 30 m/s and leaves at 300 kPa and 350 K. Determine the nozzle exit temperature [K] and pressure [kPa] of the air. The static pressure of air at the exit section for isentropic flow through the nozzle is The air at 500 kPa and 400 K enters an adiabatic nozzle at a velocity of 30 m/s and leaves at 300 kPa and 350 K. study resources. Answers: (a) 0. Not the question you’re looking for? Question: 13. Question: Air enters an adiabatic nozzle under the following conditions: pressure = 900 kPa temperature = 590 ∘∘C velocity = 2. STEAM P, = 3 MPa T = 400°C V = 40 m/s P-2. 484 K 4. Determine (a) the mass flow rate through the nozzle, (b) the exit temperature of the air, and(c) the exit area of the nozzle. close. If the air undergoes an adiabatic expansion process through. Question: Air at 640 kPa and 500 K enters an adiabatic nozzle that has an inlet-to-exit area ratio of 2:1 with a velocity of 120 m/s and leaves with a velocity of 380 m/s. This AI-generated tip is based on Chegg's full solution Question: Air @ 600 Kpa and 500 K enters an adiabatic nozzle that has an inlet to exit area ratio of 2:1 w/ a velocity of 380 m/s. 65 kPa, 153 K 17—87 Air enters a converging—diverging nozzle of a super- sonic wind tunnel at I MPa and 300 K with a low velocity. Essays; Topics; Writing Tool; plus. Accounting for the change in kinetic energy of the air, determine the change in specific flow exergy of air in this process. Air at 400 K and 500 kPa enters an adiabatic nozzle that has an inlet-to-exit area ratio of 5:1. 81, 6. The constant pressure specific heat of air at the average temperature Q2/ Air enters an adiabatic nozzle steadily at 400 kPa, 290°C, and 35 m/s and leaves at 200 kPa and 240 m/s. 5 MPa and 300°C with a low velocity and leaves at 1. The inlet area of the nozzle is 110 cm². The exit temperature of the air is 1. The inlet area of the nozzle is 80 cm². B) Air enters an adiabatic nozzle at 500 kPa and 400 K with a velocity of 80 m/s and exits at 400 kPa and 350 K (a) What is the velocity at the nozzle exit? (b) What will happen to the exit velocity if there was heat loss during the expansion? (c) Air at 500 kPa and 400 K enters an adiabatic nozzle at a velocity of 30 m/s and leaves at 300 kPa and 350 K. It exits at 200 kPa and a velocity of 151. There are 4 steps to solve this one. If the isentropic Air at 800 kPa and 400 C enters a steady-flow nozzle with a low velocity and leaves at 100 kPa. The inlet area of the nozzle is 110 cm 2. The nozzle has inlet area of 80 cm . What is the maximum velocity of Question: Air enters an adiabatic nozzle steadily at 300kPa,200∘C, and 30 m/s and leaves at 100kPa and 180 m/s. The specific heat of air at the anticipated average temperature of 450 K is cp= 1. Steam at 5 MPa and 500°C enters a nozzle steadily with a velocity of 80 m/s, and it leaves at 2 MPa and 400°C. Determine (a) the mass flow rate through the nozzle, (b) the exit 5–30 Air enters an adiabatic nozzle steadily at 300 kPa, 200°C, and 30 m/s and leaves at 100 kPa and 180 m/s. asked Jun 15, 2023 in Physics by Rutulshah ( 48. View the full answer. Approximating the flow as isentropic, calculate Air enters an adiabatic nozzle at 300 kPA, and 400 °C, and velocity of 50 m/s and exits at 85 kPA. Determine (a) the mass flow rate (m⋅), (b) the exit Problem 1: Air enters an adiabatic nozzle steadily at 300 kPa, 200°C, and 30 m/s and leaves at 100 kPa and 180 m/s. A. The inlet area of the nozzle is $80 \mathrm{~cm}^{2}$. 5304 kg/s, (b) 184. K. 3. 287 kPa. 5 The exit pressure is 325. Air enters an adiabatic nozzle at 300 kPa, 500 K with a velocity of 10 m/s. the diameter of the nozzle inlet is 4 cm. Using variable specific heats determine a) The isentropic efficiency b) The exit velocity; Air enters an adiabatic nozzle at 500 kPa, 650^{\circ}C. 0284 kJ/kg-K) (Answer: 0. 42 K. 227573 kᎫ kg K Question: air enters an adiabatic nozzle at 400 Kpa , 277C and 60 m/s and exists at 80 kpa. Determine: a) the mass flow rate through the nozzle b) the exit temperature of the air c) the exit area of the nozzle. 02 kJ/kg Determine the exit temperature. 005 kJ/kg K, %3D. The air leaves the diffuser with a velocity that is very small compared with the inlet velocity (velocity at exit condition = 0. Assume that the air is an ideal Air enters an adiabatic nozzle steadily with a pressure of 400 kPa, 500 K, and a velocity of 50 m/s. 067 kJ/kgK The negative sign indicates that the entropy decreases, which is consistent with an adiabatic nozzle. 0112 kJ/kgK C. The air at 500 kPa and 400 k enters an adiabatic nozzle with an inlet to exit area ratio of 3:2. Use variable specific heats. 02 kJ/kg. The inlet area of the diffuser is 0. Use the tables for air as an ideal gas. The nozzle isentropic efficiency is 85%. Determine (a) the mass flow rate Air enters an adiabatic nozzle at 400kPa and 547∘C with low velocity and exits at 240 m/s. 5 MPa V₂ = 300 m/s FIGURE P5-34 120 m/s and leaves with a velocity of Steam enters an adiabatic nozzle at 3. 5 m/s. The temperature and pressure of air in a large reservoir are 400 K and 3 bar respectively. The exit temperature is 605. What will happen to the nozzle exit temperature [K] and pressure [kPa] of the air if the air is cooled Question: 073) Air at 500 kPa and 400 K enters an adiabatic nozzle at avelocity of 50. Steam enters a nozzle at 400°C and 800 kPa with a velocity of 10 m/s, and leaves at 375°C and 400 kPa while losing heat at a rate of 25 kW. If the ambient state is 100 kPa and 18°C, determine ( a ) the exit velocity, ( b ) the rate of exergy destruction, and ( c ) the second-law efficiency. 02 kJ/kg. 6 MPa and 400 m/s. If the flow is ideal and exit pressure is 100 kPa, the exit temperature in K and the exit velocity in m/s are respectively? Solution: Given, Inlet pressure (P1) = 400 kPa 7–115 Air enters an adiabatic nozzle at 400 kPa and 547°C with low velocity and exits at 240 m/s. 0124 kJ/Kg| Air enters an adiabatic isentropic nozzle at 400 kPa and 547°C with a low velocity and exits at 340 m/s. Determine (a) the exit temperature and (b) the exit pressure of the air. Assuming air to be an ideal gas with constant specific heats and disregarding any irreversibilities, determine the exit velocity of the air. Air enters an adiabatic nozzle at 400 kPa and 900 K with negligible velocity. 0284 kJ/kg-K) Air enters an adiabatic nozzle steadily at 300 kPa, 200°C, and 30 m/s and leaves at 100 kPa and 180 m/s. The inlet area of the nozzle is 110 cm2. It exits the nozzle at a pressure of 100 kPa. 1. Assuming constant specific heats, determine the change in specific entropy. Determine the Mach number, pressure, and temperature of air after the expansion. Assume constant specific heats for air. The ; Air enters an adiabatic nozzle at 300 kPa, 200 C, and 30 m/s. 16: Steam flows steadily through an adiabatic turbine. Transcribed image Question: Air at 560 kPa and 400 K enters an adiabatic nozzle at a negligible velocity and leaves at 160 kPa and 350 K. It leaves the nozzle at 100 kPa with a velocity of 180 m/s. The inlet area of the nozzle is 80 cm2. 11 c. Determine (a) The isentropic efficiency (b) The exit velocity (c) The entropy generat; Air enters a nozzle steadily at 200 kPa and 65 C with a velocity of 35 m/s and exits at 95 kPa and 240 m/s. For an inlet area of 800 cm 2 , determine the velocity and the volume flow rate of the steam at the nozzle exit. determine (a) the exit temperature and (b) the exit pressure of the air. Question: 1. Changes Air enters an adiabatic nozzle at 300 kPa, 500 K with a velocity of 10 m/s. 0 m / s). Determine the exit pressure of the air Question: 5-39 Air enters an adiabatic nozzle steadily at 300 kPa, 200°C, and 45 m/s and leaves at 100 kPa and 180 m/s. Assuming air to be an ideal gas with variable specific heats and disregarding any irreversiblilities , determine ; Determine the shape of a converging-diverging nozzle for air for a mass flow rate of 3 kg/s and inlet stagnation conditions of 1400 kPa and 200^{\circ}C. 5 m/s The air leaves the nozzle at 850 kPa and 480 ∘∘C. Transcribed image text: 7-119 Air Question: Example Air at 500 kPa and 400 K enters an adiabatic nozzle at a velocity of 30 m/s and leaves at 300 kPa and 350 K. 056796 m 3 /kg, and h 2 = 275. The specific heat of air cp is 1008 J/kgKThe exit temperature of the air is Question: Air enters an adiabatic nozzle steadily at 300 kPa, 200°C, and 45 m/s and leaves at 105 kPa and 180 m/s. Question: Air at 560 kPa and 380 K enters an adiabatic nozzle at a negligible velocity and leaves at 190 kPa and 350 K What is the isentropic efficiency of the nozzle? 29. Using variable specific heats, determine $(a)$ the isentropic efficiency, $(b)$ the exit velocity, and $(c)$ the entropy generation. Using variable specific heats determine a) The isentropic efficiency b) The exit velocity; Air in a piston-cylinder undergoes a process from T_1 = 300 K and P_1 = 100 kPa to T_2 = 500 K and P_2 = 550 kPa. 5–32 Steam at 5 MPa and 400°C enters a Question: Air enters an adiabatic nozzle steadily at 300 kPa, 200°C, and 30 m/s and leaves at 100 kPa and 180 m/s. Air at 800 kPa and 400 degrees C enters a steady-flow nozzle with a low velocity and leaves at 100 k P a 100 \mathrm{kPa} 100 kPa. 7 cm 2 Solution. B Air at 600 kPa and 500 K enters an adiabatic nozzle that has an inlet-to-exit area ratio of 2:1 with a velocity of 120 m/s and leaves with a velocity of 380 m/s. Air at 500 kpa and 400K enters an adiabatic nozzle at a velocity of 30 m/s and leaves at 300 kpa and 350K. The velocity of the air stream is decreased from 230 to 30 m/s as it passes through the diffuser. Air at 600 kPa and 500 K enters an adiabatic nozzle that has an inlet-to-exit area ratio of 2:1 with a velocity of 120 m/s and leaves with a velocity of 380 m/s. To save time give the closest value in the table. If the isentropic efficiency of the nozzle is 90 percent, determine the exit temperature and pressure of the air. the exit velocity of Air at 500 kPa and 400 K enters an adiabatic nozzle at a velocity of 30 m/s and leaves at 300 kPa and 350 K. Using variable specific heats, determine (a) the exit velocity. (4 points) Air enters an adiabatic nozzle steadily at 400 kPa, 250°C, and 50 m/s and leaves at 150 kPa and 200 m/s. Air at 500 kPa and 400 K enters an adiabatic nozzle that has an inlet-to-exit area ratio of 3:1 with a velocity of 100 m/s and leaves with a velocity of 400 m/s. Compute the exit pressure and mass flows if the backpressure is, (a) 90 kPa and (b) 45 kPa. If the isentropic efficiency of the nozzle is 85 Question: Air enters an adiabatic nozzle at 400 kPa and 547 degree C with low velocity and exits at 240 m/s. The air exits at a pressure of 680 kPa and a temperature of 400 K. The inlet area of the nozzle is 100 cm. The insetropic efficiency in % B The exit velocity in m/s Air at 2 7 ∘ C and 100 kPa enters an adiabatic diffuser of a jet engine steadily with a velocity of 100 m / s. Question: 15: Air at 650 kPa and 550 K enters an adiabatic nozzle that has an inlet-to-exit area ratio of 2:1 with a velocity of 120 m/s and leaves with a velocity of 400 m/s. The exit velocity is m/s. 15- m² opening with a velocity of 30 m/s. From the refrigerant tables, v 1 = 0. For an inlet area of 800 cm 2 ^2 2, determine the velocity and the volume flow rate of the steam at the nozzle exit. 00 m/s and leaves at 300 kPa and 350 K. (Answer (a) 1. ∘C (Table A-2). Given: Air at 500 kPa and 400 K enter an adiabatic nozzle which has an inlet to exit area ratio of 3:2, the velocity of the air at the entry is 100 m/s and at the exit is 360 m/s. Using CONSTANT SPECIFIC HEATS, determine: (a) the isentropic efficiency (b) the exit velocity (c) the entropy generation Air at 80 kPa and 127 ∘ ^\circ{} ∘ C enters an adiabatic diffuser steadily at a rate of 6000 kg/h and leaves at 100 kPa. FIGURE P5-36 5-37 Reconsider Prob. 5 kg/s where it is mixed Refrigerant-134a at 700 kPa and 120°C enters an adiabatic nozzle steadily with a velocity of 18 m/s and leaves at 400 kPa and 30°C. To solve this problem, we can use the principle of conservation of mass and the adiabatic flow equation. Determine (a) the mass flow rate through the nozzle, (b) the exit temperature of the air, and (c) the exit area of the nozzle. 5 MPa V, 300 m/s 2- Air at 80 kPa, 27°C, and 220 m/s enters a Air at 500 kPa and 400 K enters an adiabatic nozzle at a velocity of 30 m/s and leaves at 300 kPa and 350 K. Thermodynamics 5-39Air enters an adiabatic nozzle steadily at 300 kPa, 200°C, and 45 m/s and leaves at 100 kPa and 180 m/s. To determine the Q2/ Air enters an adiabatic nozzle steadily at 400 kPa, 290°C, and 35 m/s and leaves at 200 kPa and 240 m/s. 00 \mathrm{~m} / \mathrm{s} \) and leaves at 300 kPa and 350 K . Determine the velocity (m/s) at the exit of the diffuser. Determine the entropy generation in (kJ/kg K) 1) Air enters an adiabatic nozzle steadily at 300 Kpa, 200 {eq}^o{/eq}C, and 45 m/s and leaves at 100 kPa and 180 m/s. Refrigerant- 134 a at 700 kPa and 120 degree C enters an adiabatic 1. 0. 925 m/s c) 0. mp/kg. (b) the exit velocity, and (c) the entropy generation. Air enters an adiabatic nozzle at 400 kpa , 277 o C and 60 m/s and exist at 80 kPa . If the isentropic efficiency of the nozzle is 90 percent, determine the exit temperature and pressure Air enters an adiabatic nozzle steadily at 300 kPa, 200°C, and 30 m/s and leaves at 100 kPa and 180 m/s. The compressor pressure ratio is 9, the turbine inlet temperature is 1400 K, and air exits the nozzle at 26 kPa. Determine the exit velocity. If the air undergoes an adiabatic expansion process through the nozzle, what is the maximum velocity of the air at the nozzle exit in $\mathrm{m} / \mathrm{s}$ ?. 8552 m/s. Air at 600 kPa and 500 K enters an adiabatic nozzle that has an inlet-to-exit area ratio of 2: 1 with a velocity of 120 m / s and leaves with a velocity of 380 m / s. 073. a) Assuming an isentropic efficiency of 85%, and negligible inlet velocity, calculate the exit temperature, area, Air enters an adiabatic nozzle at 400 kpa , 277 o C and 60 m/s and exist at 80 kPa The air at 500 kPa and 400 K enters an adiabatic nozzle at a velocity of 30 m/s and leaves at 300 kPa and 350 K. Comprehension Air enters an adiabatic nozzle at 300 kPa, 500 K with a velocity of 10 m/s. Use variablespecific heats. Here’s how to approach this question. If the nozzle inlet has an area = 88 cm^2, what is the area of the ; Oxygen at 300 kPa and 90 degrees C flowing at an average velocity of 3 m/s is expanded in an adiabatic nozzle. (a) the The air at 500 kPa and 400 K enters an adiabatic nozzle at a velocity of 30 m/s and leaves at 300 kPa and 350 K. Previous question Next question. A hot-water stream at 80°C enters a mixing chamber with a mass flow rate of 0. 07. The inlet area of the nozzle is 100 Skip to main content. Homework Help is Here – Start Your Trial Now! arrow_forward. zchl oeyyj rjjs byiukecs duml qsdc wbhqwra blhvz sklo zexhq