1. Date of download: 7/6/2016 Copyright © ASME. All rights reserved. From: On the Design of an Aero-Engine Nose Cone Anti-Icing System Using a Rotating Heat Pipe J. Thermal Sci. Eng. Appl. 2009;1(2):022002-022002-11. doi:10.1115/1.4000191 Schematic of proposed rotating heat pipe anti-icing system Figure Legend:

2. Date of download: 7/6/2016 Copyright © ASME. All rights reserved. From: On the Design of an Aero-Engine Nose Cone Anti-Icing System Using a Rotating Heat Pipe J. Thermal Sci. Eng. Appl. 2009;1(2):022002-022002-11. doi:10.1115/1.4000191 Schematic showing coordinate system for modeling of rotating heat pipe Figure Legend:

3. Date of download: 7/6/2016 Copyright © ASME. All rights reserved. From: On the Design of an Aero-Engine Nose Cone Anti-Icing System Using a Rotating Heat Pipe J. Thermal Sci. Eng. Appl. 2009;1(2):022002-022002-11. doi:10.1115/1.4000191 Heat transfer rate through the anti-icing system using — water and - - - ethanol as the working fluid in the heat pipe at airplane speeds of V= ◇ 300 km/h and △ 600 km/h Figure Legend:

4. Date of download: 7/6/2016 Copyright © ASME. All rights reserved. From: On the Design of an Aero-Engine Nose Cone Anti-Icing System Using a Rotating Heat Pipe J. Thermal Sci. Eng. Appl. 2009;1(2):022002-022002-11. doi:10.1115/1.4000191 Effect of atmospheric air temperature on the surface temperature of the nose cone using water at Tamb= ◇ -5°C, △ -10°C, ×-20°C, and ○-30°C for ω=5000 rpm and V=300 km/h Figure Legend:

5. Date of download: 7/6/2016 Copyright © ASME. All rights reserved. From: On the Design of an Aero-Engine Nose Cone Anti-Icing System Using a Rotating Heat Pipe J. Thermal Sci. Eng. Appl. 2009;1(2):022002-022002-11. doi:10.1115/1.4000191 Effect of working fluid on surface temperature of the nose cone using — water and - - - ethanol at ω=○ 5000 rpm, × 10,000 rpm, △ 15,000 rpm, and ◇ 20,000 rpm for V=300 km/h and Tamb=−30°C Figure Legend:

6. Date of download: 7/6/2016 Copyright © ASME. All rights reserved. From: On the Design of an Aero-Engine Nose Cone Anti-Icing System Using a Rotating Heat Pipe J. Thermal Sci. Eng. Appl. 2009;1(2):022002-022002-11. doi:10.1115/1.4000191 Effect of airplane speed on the surface temperature of the nose cone using water at V=300 km/h: ● 5000 rpm, ◆ 20,000 rpm and V=600 km/h: ○ 5000 rpm, ◇ 20000 rpm for Tamb=−30°C Figure Legend:

7. Date of download: 7/6/2016 Copyright © ASME. All rights reserved. From: On the Design of an Aero-Engine Nose Cone Anti-Icing System Using a Rotating Heat Pipe J. Thermal Sci. Eng. Appl. 2009;1(2):022002-022002-11. doi:10.1115/1.4000191 Effect of heating channels on the surface temperature of the nose cone using water with ◆ 10 insulated channels, ◇ 10, △ 50, and ○ 100 active channels for ω=5000 rpm and Tamb=−30°C Figure Legend:

8. Date of download: 7/6/2016 Copyright © ASME. All rights reserved. From: On the Design of an Aero-Engine Nose Cone Anti-Icing System Using a Rotating Heat Pipe J. Thermal Sci. Eng. Appl. 2009;1(2):022002-022002-11. doi:10.1115/1.4000191 Thermal resistance representation of the anti-icing system Figure Legend: