FUNDAMENTALS OF THERMODYNAMICS
10th Edition
ISBN: 9781119634928
Author: Borgnakke
Publisher: WILEY
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Topic: Ideal gas process
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Find the velocity (in ft/s) at a second point a short distance away, where the pressure is
83 psia, from the isentropic flow of nitrogen gas in a 2-in-ID pipe. At the first point, the
velocity is 409 ft/sec, pressure is 85 psia, and unit weight is 0.655 lb/ft³
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- Finding exit temperature in F, and volumetric flow rate. Step by step solution please thank youuuarrow_forwardAn isobaric steam generating process starts with saturated liquid at 20 psia. The change in entropy is equal to the initial entropy. What is the change in enthalpy during the process? (Hint: not all of the liquid is vaporized)A. -230.4 Btu/lbmB. -196.2 Btu/lbmC. 196.2 Btu/lbmD. 230.4 Btu/lbmarrow_forward20. If 10 kg/min of air are compressed isothermally from P1 = 96 kPa and Vi 7.65 m³/min to P2 = 620 kPa, find the work, change in entropy %3D for a non-flow process and a steady flow process with vị = 15 m/s and v2 = 60 m/s.arrow_forward
- p61#6. Carbon Dioxide at p₁ = 500 psia,v₁ = ft/min, and t₁ = 200°F are cooled at constant volume to 130°F in an internally reversible manner. For m=0.9 lbm/min, determine in ∫pdv and -∫vdp. For nonflow process, find p2, change of internal energy, change of enthalpy, and Q. Also, compute change of entropy.arrow_forwardPlease help with detailed solution.arrow_forward*** ***Solve the following problems, correctly and systematically, and show all the necessary figures. Show your correct and complete solution neatly. There are required 2000 kW of compressor power to handle air adiabatically from 1 atmosphere, 27 °C, to 305 kPaa. The initial air velocity is 20 m/s and the final velocity is 85 m/s. a) If the compression is isentropic, find the compressor capacity, in m3/s. b) If the compression process is irreversible adiabatic to a temperature of 160 °C, with the capacity found in (a), determine the compressor power input, in Hp.arrow_forward
- 2) In a steady flow of air through a nozzle, the enthalpy decreases by 40 kj. Assuming there is no other energy changes other than KE det the velocity at sec 2, if the vel at sec 1 is 100 m/sarrow_forwardSketch and label the nozzle. Sketch and label the process on a P-v diagram, also mention all numbers on the process of P-V diagram please. 7.15 The exit nozzle in a jet engine receives air at 1200 K, 150 kPa with negligible kinetic energy. The exit pressure is 80 kPa, and the process is reversible and adiabatic. Use constant specific heat at 300 K to find the exit velocity.arrow_forwardPlease show your complete solution. Thank you! During the reversible process executed by the non-flow system, the pressure increases 334.79 kPa to 1378.96 kPa in accordance with PV=C and the internal energy increase is 22, 577 J, the initial volume is 85 liters. Find the heat.arrow_forward
- Air enters a turbine at temperature and pressure of 800°C, 10bar respectively. The actual exit airtemperature is 180°C. The turbine isentropic efficiency is estimated to be 85%. Calculate the turbine exit pressure and the actual expansion index (n).arrow_forwardPLEASE ANSWER WITH COMPLETE SOLUTION AND DIAGRAM.arrow_forwardA confined volume of 27 moles an ideal gas (with y = 1.42) goes through an expansion process so at the final volume is six times the initial volume, and the final pressure is one eighth the initial ressure. a. What is the final temperature in terms of the initial temperature? b. What is the total change in entropy for the gas?arrow_forward
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