[1]
Boudlal, A., Ghezali, F. and Lahcene, A. 2025. An Evaluation of the Performance of a Novel Film Cooling Holes applied to Gas Turbine Blades. Engineering, Technology & Applied Science Research. 15, 3 (Jun. 2025), 22306–22311. DOI:https://doi.org/10.48084/etasr.10472.