Air enters a cooling section at 97 kPa, 35°C, and 30 percent relative humidity at a rate of 6 m3/min, where it is cooled until the moisture in the air starts condensing. Determine (a) the temperature of the air at the exit and (b) the rate of heat transfer in the cooling section.
(a)
The temperature of the air at the exit.
Answer to Problem 130RP
The temperature of the air at the exit is
Explanation of Solution
As the process is a steady flow and thus the mass flow rate of dry air remains constant during the entire process.
Here, the mass flow rate of air at inlet is
The amount of moisture in the air remains constant as it flows through the heating section as process involves no dehumidification or humidification.
Here, specific humidity at state 1 and 2 is
Express initial partial pressure.
Here, relative humidity at state 1 is
Express initial humidity ratio.
Here, pressure at state 1 is
Express initial enthalpy.
Here, specific heat at constant pressure is
Express specific volume at state 1.
Here, gas constant of air is
As the air at the final state is saturated and the vapor pressure during the process will remain constant, thus the dew point temperature is the exit temperature.
Here, exit temperature is
Conclusion:
Refer Table A-4, “saturated water-temperature table”, and write the saturation pressure and initial specific enthalpy saturated vapor at temperature of
Substitute
Substitute
Substitute
Refer Table A-2, “ideal-gas specific heats of various common gases”, and write the properties of air.
Substitute
Substitute
Substitute
Refer Table A-5, “saturated water-pressure table”, and write the saturation temperature or exit temperature at pressure of
Write the formula of interpolation method of two variables.
Here, the variables denote by x and y is pressure and exit or saturation temperature respectively.
Show the specific enthalpy at state 2 corresponding to specific entropy as in Table (1).
Pressure |
Saturation or exit temperature |
1.5 | 13.02 |
1.69 | |
2 | 17.50 |
Substitute
Substitute
Hence, the temperature of the air at the exit is
(b)
The rate of heat transfer in the cooling section.
Answer to Problem 130RP
The rate of heat transfer in the cooling section is
Explanation of Solution
Express the enthalpy of air at exit.
Here, temperature at exit is
Express mass flow rate of air.
Here, volume flow rate at inlet is
Express the rate of heat transfer in the cooling section.
Conclusion:
Refer Table A-4, “saturated water-temperature table”, and write the final specific enthalpy saturated vapor at temperature of
Show the final specific enthalpy saturated vapor corresponding to exit temperature as in Table (2).
Exit temperature |
Final specific enthalpy saturated vapor |
10 | 2519.2 |
14.8 | |
15 | 2528.3 |
Use excels and tabulates the values from Table (2) in Equation (VIII) to get,
Substitute
Substitute
Substitute
Substitute
Hence, the rate of heat transfer in the cooling section is
Want to see more full solutions like this?
Chapter 14 Solutions
Thermodynamics: An Engineering Approach ( 9th International Edition ) ISBN:9781260092684
- Generate the kinematic diagram of the following mechanisms using the given symbols. Then, draw their graphs and calculate their degrees of freedom (DoF) using Gruebler's formula. PUNTO 2. PUNTO 3. !!!arrow_forwardCreate a schematic representation of the following mechanisms using the given symbols and draw their graphs. Then, calculate their degrees of freedom (DoF) using Gruebler's formula. PUNTO 6. PUNTO 7.arrow_forwardhow the kinematic diagram of the following mechanisms would be represented using the given symbols? PUNTO 0. PUNTO 1. °arrow_forward
- Create a schematic representation of the following mechanisms using the given symbols and draw their graphs. Then, calculate their degrees of freedom (DOF) using Gruebler's formula. PUNTO 4. PUNTO 5. (0) Groundarrow_forwardDraw the graph of ALL the mechanisms and calculate their DoF using Gruebler's formula. PUNTO 0. PUNTO 1.arrow_forwardAn adjustable support. Construction designed to carry vertical load and is adjusted by moving the blue attachment vertically. The link is articulated at both ends (free to rotate) and can therefore only transmit power axially. Analytically calculate the force to which the link is subjected? Calculate analytically rated voltage in the middle of the link.? F=20kN Alpha 30 deg Rel 225 Mpans:5arrow_forward
- A swivel crane where the load is moved axially along the beam through the wagon to which the hook is attached. Round bar with a diameter of ∅30 mm. The support beam is articulated at both ends (free to rotate) and can therefore only transmit force axially. Calculate reaction force in the x-direction at point A? Calculate analytical reaction force in the y-direction of point A? Calculate nominal stress in the middle of the support beam?Lengt 5 mAlfa 25 degX=1.5mIPE300-steelmass:1000 kgarrow_forwardgot wrong answers help pleasearrow_forwardA crate weighs 530 lb and is hung by three ropes attached to a steel ring at A such that the top surface is parallel to the xy plane. Point A is located at a height of h = 42 in above the top of the crate directly over the geometric center of the top surface. Use the dimensions given in the table below to determine the tension in each of the three ropes. 2013 Michael Swanbom cc00 BY NC SA ↑ Z C b B У a D Values for dimensions on the figure are given in the following table. Note the figure may not be to scale. Variable Value a 30 in b 43 in 4.5 in The tension in rope AB is 383 x lb The tension in rope AC is 156 x lb The tension in rope AD is 156 x lbarrow_forward
- A block of mass m hangs from the end of bar AB that is 7.2 meters long and connected to the wall in the xz plane. The bar is supported at A by a ball joint such that it carries only a compressive force along its axis. The bar is supported at end B by cables BD and BC that connect to the xz plane at points C and D respectively with coordinates given in the figure. Cable BD is elastic and can be modeled as a linear spring with a spring constant k = 400 N/m and unstretched length of 6.34 meters. Determine the mass m, the compressive force in beam AB and the tension force in cable BC. Z C D (c, 0, d) (a, 0, b) A B y f m cc 10 BY NC SA 2016 Eric Davishahl x Values for dimensions on the figure are given in the following table. Note the figure may not be to scale. Variable Value a 8.1 m b 3.3 m с 2.7 m d 3.9 m e 2 m f 5.4 m The mass of the block is 68.8 The compressive force in bar AB is 364 × kg. × N. The tension in cable BC is 393 × N.arrow_forwardThe airplane weighs 144100 lbs and flies at constant speed and trajectory given by 0 on the figure. The plane experiences a drag force of 73620 lbs. 0 a.) If 11.3°, determine the thrust and lift forces = required to maintain this speed and trajectory. b.) Next consider the case where is unknown, but it is known that the lift force is equal to 7.8 times the quantity (Fthrust Fdrag). Compute the resulting trajectory angle and the lift force in this case. Use the same values for the weight and drag forces as you used for part a. 20. YAAY' Farag Ө Fthrust CC + BY NC SA 2013 Michael Swanbom Flift Fweight The lift force acts in the y' direction. The weight acts in the negative y direction. The thrust and drag forces act in the positive and negative x' directions respectively. Part (a) The thrust force is equal to 101,855 ☑ lbs. The lift force is equal to 141,282 ☑ lbs. Part (b) The trajectory angle 0 is equal to 7.31 ✓ deg. The lift force is equal to 143,005 ☑ lbs.arrow_forwardsimply supported beam has a concentrated moment M, applied at the left support and a concentrated force F applied at the free end of the overhang on the right. Using superposition, determine the deflection equations in regions AB and BC.arrow_forward
- Elements Of ElectromagneticsMechanical EngineeringISBN:9780190698614Author:Sadiku, Matthew N. O.Publisher:Oxford University PressMechanics of Materials (10th Edition)Mechanical EngineeringISBN:9780134319650Author:Russell C. HibbelerPublisher:PEARSONThermodynamics: An Engineering ApproachMechanical EngineeringISBN:9781259822674Author:Yunus A. Cengel Dr., Michael A. BolesPublisher:McGraw-Hill Education
- Control Systems EngineeringMechanical EngineeringISBN:9781118170519Author:Norman S. NisePublisher:WILEYMechanics of Materials (MindTap Course List)Mechanical EngineeringISBN:9781337093347Author:Barry J. Goodno, James M. GerePublisher:Cengage LearningEngineering Mechanics: StaticsMechanical EngineeringISBN:9781118807330Author:James L. Meriam, L. G. Kraige, J. N. BoltonPublisher:WILEY