Pulsed film cooling was studied experimentally to determine its effect on film cooling effectiveness. The film cooling jets were pulsed using solenoid valves in the supply air line. Cases with a single row of cylindrical film cooling holes inclined at 35 degrees to the surface of a flat plate were considered at blowing ratios of 0.25, 0.5, 1.0, and 1.5 for a variety of pulsing frequencies and duty cycles. Temperature measurements were made using an infrared camera, thermocouples, and cold wire anemometry. Hot wire anemometry was used for velocity measurements. The local film cooling effectiveness was calculated based on the measured temperatures and the results were compared to baseline cases with continuous blowing. Phase locked flow temperature fields were determined from cold wire surveys. Pulsing at high frequencies helped to improve film cooling effectiveness in some cases by reducing overall jet liftoff. At lower frequencies, pulsing tended to have the opposite effect. With the present geometry and a steady mainflow, pulsing did not provide an overall benefit. The highest overall effectiveness was achieved with continuous jets and a blowing ratio of 0.5. The present results may prove useful for understanding film cooling behavior in engines, where mainflow unsteadiness causes film cooling jet pulsation.
Skip Nav Destination
ASME Turbo Expo 2006: Power for Land, Sea, and Air
May 8–11, 2006
Barcelona, Spain
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
0-7918-4238-X
PROCEEDINGS PAPER
Effect of Jet Pulsing on Film Cooling: Part 1— Effectiveness and Flowfield Temperature Results
Sarah M. Coulthard,
Sarah M. Coulthard
Stanford University, Stanford, CA
Search for other works by this author on:
Ralph J. Volino,
Ralph J. Volino
U.S. Naval Academy, Annapolis, MD
Search for other works by this author on:
Karen A. Flack
Karen A. Flack
U.S. Naval Academy, Annapolis, MD
Search for other works by this author on:
Sarah M. Coulthard
Stanford University, Stanford, CA
Ralph J. Volino
U.S. Naval Academy, Annapolis, MD
Karen A. Flack
U.S. Naval Academy, Annapolis, MD
Paper No:
GT2006-91273, pp. 1083-1094; 12 pages
Published Online:
September 19, 2008
Citation
Coulthard, SM, Volino, RJ, & Flack, KA. "Effect of Jet Pulsing on Film Cooling: Part 1— Effectiveness and Flowfield Temperature Results." Proceedings of the ASME Turbo Expo 2006: Power for Land, Sea, and Air. Volume 3: Heat Transfer, Parts A and B. Barcelona, Spain. May 8–11, 2006. pp. 1083-1094. ASME. https://doi.org/10.1115/GT2006-91273
Download citation file:
12
Views
0
Citations
Related Proceedings Papers
Related Articles
Effect of Jet Pulsing on Film Cooling—Part I: Effectiveness and Flow-Field Temperature Results
J. Turbomach (April,2007)
Effect of Jet Pulsing on Film Cooling—Part II: Heat Transfer Results
J. Turbomach (April,2007)
Distortion in Thermal Field Around Inserted Thermocouples in Experimental Interfacial Studies, Part 4: End Effect
J. Manuf. Sci. Eng (February,2002)
Related Chapters
Completing the Picture
Air Engines: The History, Science, and Reality of the Perfect Engine
Outlook
Closed-Cycle Gas Turbines: Operating Experience and Future Potential
Control and Operational Performance
Closed-Cycle Gas Turbines: Operating Experience and Future Potential