Net heat flux reduction for pulsed film cooling on a turbine blade leading edge

Authors

James L. Rutledge, Air Force Institute of TechnologyFollow
Paul I. King, Air Force Institute of Technology
Richard B. Rivir, Air Force Research Laboratory

Document Type

Conference Proceeding

Publication Date

8-2-2009

Comments

Co-author J. Rutledge was an AFIT PhD candidate at the time of this paper. (AFIT-DS-ENY-09-S03, September 2009)

Conference Session: GTE-14: Heat Transfer I - Film Cooling

DOI

10.2514/6.2009-5103

Source Publication

AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 45th

Recommended Citation

Rutledge, J., King, P., & Rivir, R. (2009, August 2). Net heat flux reduction for pulsed film cooling on a turbine blade leading edge. 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Denver, Colorado. https://doi.org/10.2514/6.2009-5103