1. Date of download: 10/3/2017
Copyright © ASME. All rights reserved.
From: Theoretical and Experimental Investigations of Solar-Thermoelectric Air-Conditioning System for Remote Applications
J. Thermal Sci. Eng. Appl. 2015;7(2): doi: /
Figure Legend:
Schematic diagram of the TE air-conditioning module with different components and power supply

2. Date of download: 10/3/2017
Copyright © ASME. All rights reserved.
From: Theoretical and Experimental Investigations of Solar-Thermoelectric Air-Conditioning System for Remote Applications
J. Thermal Sci. Eng. Appl. 2015;7(2): doi: /
Figure Legend:
Heat removal QL as a function of input current i at different values of unit TE cell at (A0U0)cond=18 W/K, (A0U0)eva=1.2 W/K, TL = 298 K, and TH = 298 K

3. Date of download: 10/3/2017
Copyright © ASME. All rights reserved.
From: Theoretical and Experimental Investigations of Solar-Thermoelectric Air-Conditioning System for Remote Applications
J. Thermal Sci. Eng. Appl. 2015;7(2): doi: /
Figure Legend:
Heat removal QL as a function of input current i at different temperature difference at TH = 320 K

4. Date of download: 10/3/2017
Copyright © ASME. All rights reserved.
From: Theoretical and Experimental Investigations of Solar-Thermoelectric Air-Conditioning System for Remote Applications
J. Thermal Sci. Eng. Appl. 2015;7(2): doi: /
Figure Legend:
Heat removal QL as a function of temperature difference ΔT between the high and low temperature reservoir at different values of temperatures at high temperature reservoir (i = 1 A)

5. Date of download: 10/3/2017
Copyright © ASME. All rights reserved.
From: Theoretical and Experimental Investigations of Solar-Thermoelectric Air-Conditioning System for Remote Applications
J. Thermal Sci. Eng. Appl. 2015;7(2): doi: /
Figure Legend:
Effect of temperature difference ΔT on the power input Pin to the system at different values of ambient temperature TH a fixed current i = 3.0 A

6. Date of download: 10/3/2017
Copyright © ASME. All rights reserved.
From: Theoretical and Experimental Investigations of Solar-Thermoelectric Air-Conditioning System for Remote Applications
J. Thermal Sci. Eng. Appl. 2015;7(2): doi: /
Figure Legend:
COP as a function of input current i at different numbers of unit module at TH = 310 K and TL = 290 K

7. Date of download: 10/3/2017
Copyright © ASME. All rights reserved.
From: Theoretical and Experimental Investigations of Solar-Thermoelectric Air-Conditioning System for Remote Applications
J. Thermal Sci. Eng. Appl. 2015;7(2): doi: /
Figure Legend:
COP as a function of temperature difference ΔT at different ambient temperatures TH and the current input i = 3.0 A

8. Date of download: 10/3/2017
Copyright © ASME. All rights reserved.
From: Theoretical and Experimental Investigations of Solar-Thermoelectric Air-Conditioning System for Remote Applications
J. Thermal Sci. Eng. Appl. 2015;7(2): doi: /
Figure Legend:
Schematic diagram of the experimental setup with different components

9. Date of download: 10/3/2017
Copyright © ASME. All rights reserved.
From: Theoretical and Experimental Investigations of Solar-Thermoelectric Air-Conditioning System for Remote Applications
J. Thermal Sci. Eng. Appl. 2015;7(2): doi: /
Figure Legend:
Temperature variation in the conditioned space with time when ∀·eva = 30 m3/h, ∀·cond = 32.5 m3/h, Cv = 0.718 kJ/kg·K, ρair = 1.184 kg/m3, n = 120, (A0U0)con = 3.87 W/K, (A0U0)eva=0.32 W/K, and T0 = 0°C

10. Date of download: 10/3/2017
Copyright © ASME. All rights reserved.
From: Theoretical and Experimental Investigations of Solar-Thermoelectric Air-Conditioning System for Remote Applications
J. Thermal Sci. Eng. Appl. 2015;7(2): doi: /
Figure Legend:
Temperature variation in the conditioned space with time when ∀·eva = 30 m3/h, ∀·cond = 32.5 m3/h, Cv = 0.718 kJ/kg·K, ρair = 1.184 kg/m3, n = 120, (A0U0)con = 3.87 W/K, (A0U0)eva=0.32 W/K, and T0 = 15°C

11. Date of download: 10/3/2017
Copyright © ASME. All rights reserved.
From: Theoretical and Experimental Investigations of Solar-Thermoelectric Air-Conditioning System for Remote Applications
J. Thermal Sci. Eng. Appl. 2015;7(2): doi: /
Figure Legend:
Temperature variation in the conditioned space with time when ∀·eva = 30 m3/h, ∀·cond = 32.5 m3/h, Cv = 0.718 kJ/kg·K, ρair = 1.184 kg/m3, n = 120, (A0U0)con = 3.87 W/K, (A0U0)eva = 0.32 W/K, and T0 = 17°C with nonzero internal heat load