FUNDAMENTALS OF THERMODYNAMICS
10th Edition
ISBN: 9781119634928
Author: Borgnakke
Publisher: WILEY
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Air enters a diffuser at 50 kPa, 85°C with a velocity of 250 m/s. The exit pressure is atmospheric at 101 kPa. The exit temperature is 110°C. The diameter at the inlet is 8 cm.a. Find the exit velocity.b. Find the diameter at the exit.Note: Assume constant specific heats.
Steam enters a nozzle at pressure of 1 MPa,
temperature of 500 °C, and a velocity of 38 m/s and
leaves as saturated vapor at 75 kPa, what is the exit
velocity (m/s) when a heat loss of 19.5 kJ/kg is
present?
7. If 10 kg/min of air are compressed isothermally from
= 96 kPa and V, = 7.65 m/min to p, = 620 kPa, find the work,
the change of entropy and the heat for (a) nonflow process and
b) a steady flow process with v, = 15 m/s and v, = 60 m/s.
Ans. (a)-1370KJ/min,-5.356 kJ/K.min; (b)-1386.9kJ,
%3D
min
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- occuring when a process with air, the entropy goes up by 0.60 kJ/kg·K. 11 is the pressure compression ratio. 300K is the initial temperature. What is the final temperature if it is a constant specific heat and if it is a variable specific heat? When Rair = 0.287 and cp = 1.005 kJ/kg·K.arrow_forwardSolve it correctly please. I will rate. Answer should be matcharrow_forwardAir 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_forward
- During a process with air, the entropy increases by 0.55 kJ/(kg·K). The pressure compression ratio is 10 and the initial temperature is 300K. Find the final temperature assuming a) constant heat capacities and b) variable heat capacities? (Rair = 0.287 and cp = 1.005 kJ/kg·K)arrow_forwardTopic: Ideal gas process Instructions: Answer the following review questions and show complete solutions. *please write legibly. Thank youarrow_forwardAir enters a blower at 20°C and exits at 28.38°C. The inlet velocities of air are 100 m/s and 150 m/s respectively. Find the mass flow rate if the blower consumes a power of 15 kW, assuming adiabaticconditions. Take cp of air is 1.005 kJ/kg-K. Need answers and solutions. ASAP...arrow_forward
- I need the answer as soon as possiblearrow_forwardQ3. An internal combustion engine consumes 6 kg of fuel per hour, ip of engine is 27 kW and mechanical efficiency is 80%. It uses 12 kg of cooling water per minute and the inlet and outlet temperature of water being 18 °C and 48 °C respectively. The exhaust gases raise the temperature of 8.4 kg/ water through 32 °C. The orific value of fuel used is 44 MJ/kg. Calculate the indicated thermal efficiency, overall efficiency of the engine and draw heat balance sheet.arrow_forwarda- In the fig shown air entering a diffuser at 70 kpa , 27 °C , with a velocity of 100 m/s. and leaves at 20 m/s. If Air the inlet cross section area of 1cm? and the outlet 8.6 cm determine the exit pressure and temperature of air.( 1 kJ/kg = 1,000 m/s²) consider the case of ideal gas and CP = 1.004 kJ/kg.arrow_forward
- p91#16. 1000CFM of air are compressed at constant tem,perature of 85 degree farenheit and 198psia to 580psia. for both nonflow and steadyflow, compute integral fo pdv, -integral of Vdp, change in entropy and change in enthalpyarrow_forwardp61#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_forwardQ 3 A nozzle shown in Fig. Q 3, receives steam at 7 bar and 200°C and expands it reversibly and adiabatically (i.e., isentropically) into a space at 3 bar where its quality or dryness fraction is 98%. Neglecting the inlet velocity, calculate the exit diameter required for a mass flow rate of 0.1 kg/s. Inlet-1 Exit-2 V, »V, V Convergent-divergent nozzle Insulation Control surface Figure for Q 3arrow_forward
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