Experimental study of subsonic film cooling performance in aircraft engine gas turbine blades via thermal paint, Laser Doppler Anemometry (LDA) and thermal wind tunnel techniques
Presentation / Conference
Beg, O., Daud, H., Beg, T., Kadir, A., Leonard, H., & Malysheva, L. Experimental study of subsonic film cooling performance in aircraft engine gas turbine blades via thermal paint, Laser Doppler Anemometry (LDA) and thermal wind tunnel techniques. Presented at ICFMA 2022: 16th International Conference on Fluid Mechanics and Applications, Lisbon, Portugal
The present study employs thermal paint technology (TPT) to investigate the performance of holes arrays on gas turbine film cooling. Detailed tests have been performed to study the influence of blowing ratio (BR) and angle of injection on realistic g... Read More about Experimental study of subsonic film cooling performance in aircraft engine gas turbine blades via thermal paint, Laser Doppler Anemometry (LDA) and thermal wind tunnel techniques.