Date of download: 11/9/2017 Copyright © ASME. All rights reserved. From: Influence of Coolant Jet Pulsation on the Convective Film Cooling of an Adiabatic Wall J. Heat Transfer. 2016;139(2):022201-022201-12. doi:10.1115/1.4034773 Figure Legend: (a) Schematic diagram of injection flow system, R(0-1): pressure regulator, T0: temperature probe PT100, T(1-2) thermocouple type-K, (b) experimental arrangement for infrared thermography

Date of download: 11/9/2017 Copyright © ASME. All rights reserved. From: Influence of Coolant Jet Pulsation on the Convective Film Cooling of an Adiabatic Wall J. Heat Transfer. 2016;139(2):022201-022201-12. doi:10.1115/1.4034773 Figure Legend: Heat transfer model, using a linear fit for four points

Date of download: 11/9/2017 Copyright © ASME. All rights reserved. From: Influence of Coolant Jet Pulsation on the Convective Film Cooling of an Adiabatic Wall J. Heat Transfer. 2016;139(2):022201-022201-12. doi:10.1115/1.4034773 Figure Legend: Comparison of time-averaged profiles of U/U∞, lying at x/d = 3.5 and 5.5 of the hole central plane (z/d = 0), for different St (0, 0.2 0.3 and 0.5) examined under a range of M (0.65, 1 and 1.25), while M increasing columnwise and x/d increasing rowwise

Date of download: 11/9/2017 Copyright © ASME. All rights reserved. From: Influence of Coolant Jet Pulsation on the Convective Film Cooling of an Adiabatic Wall J. Heat Transfer. 2016;139(2):022201-022201-12. doi:10.1115/1.4034773 Figure Legend: Steady blowing results for adiabatic effectiveness: (a) M= 0.65, (b) M= 1, (c) M= 1.25 and convective heat transfer coefficient: (d) M= 0.65, (e) M= 1, and (f) M= 1.25

Date of download: 11/9/2017 Copyright © ASME. All rights reserved. From: Influence of Coolant Jet Pulsation on the Convective Film Cooling of an Adiabatic Wall J. Heat Transfer. 2016;139(2):022201-022201-12. doi:10.1115/1.4034773 Figure Legend: Film cooling at Ti/T∞=2, centerline effectiveness: (a) M= 0.65, (b) M= 1, (c) M= 1.25, and laterally averaged effectiveness: (d) M= 0.65, (e) M= 1, and (f) M= 1.25

Date of download: 11/9/2017 Copyright © ASME. All rights reserved. From: Influence of Coolant Jet Pulsation on the Convective Film Cooling of an Adiabatic Wall J. Heat Transfer. 2016;139(2):022201-022201-12. doi:10.1115/1.4034773 Figure Legend: Film cooling at Ti/T∞=2, centerline heat transfer coefficient (a) M= 0.65, (b) M= 1, (c) M= 1.25, and laterally averaged heat transfer coefficient (d) M= 0.65, (e) M= 1, and (f) M= 1.25

Date of download: 11/9/2017 Copyright © ASME. All rights reserved. From: Influence of Coolant Jet Pulsation on the Convective Film Cooling of an Adiabatic Wall J. Heat Transfer. 2016;139(2):022201-022201-12. doi:10.1115/1.4034773 Figure Legend: Comparison of film cooling parameters blowing at Ti/T∞=2, (a) centerline adiabatic effectiveness and (b) centerline Stanton number ratio

Date of download: 11/9/2017 Copyright © ASME. All rights reserved. From: Influence of Coolant Jet Pulsation on the Convective Film Cooling of an Adiabatic Wall J. Heat Transfer. 2016;139(2):022201-022201-12. doi:10.1115/1.4034773 Figure Legend: Comparison of the laterally averaged heat transfer coefficient in the immediate downstream region

Date of download: 11/9/2017 Copyright © ASME. All rights reserved. From: Influence of Coolant Jet Pulsation on the Convective Film Cooling of an Adiabatic Wall J. Heat Transfer. 2016;139(2):022201-022201-12. doi:10.1115/1.4034773 Figure Legend: Wall zone for estimating spatially averaged results

Date of download: 11/9/2017 Copyright © ASME. All rights reserved. From: Influence of Coolant Jet Pulsation on the Convective Film Cooling of an Adiabatic Wall J. Heat Transfer. 2016;139(2):022201-022201-12. doi:10.1115/1.4034773 Figure Legend: Comparison of different cases of pulsation, Ti/T∞=2, (a) spatially averaged effectiveness and (b) spatially averaged heat transfer coefficient

Date of download: 11/9/2017 Copyright © ASME. All rights reserved. From: Influence of Coolant Jet Pulsation on the Convective Film Cooling of an Adiabatic Wall J. Heat Transfer. 2016;139(2):022201-022201-12. doi:10.1115/1.4034773 Figure Legend: Film cooling at Ti/T∞=2, centerline NHFR (a) M= 0.65, (b) M= 1, (c) M= 1.25, and laterally averaged NHFR (d) M=0.65, (e) M= 1, and (f) M= 1.25