STRONGLY HEATED TURBULENT BOUNDARY LAYER IN A CHANNEL WITH STAGGERED PIN FINS

von Lee, Chien-Shing
Veröffentlicht in AIAA Propulsion and Energy Forum (2019 : Indianapolis, Ind.) Gas turbine engines ; Volume 2 of 2 (2019)

GT2020-14317: Downstream Vortex Generators to Enhance Film-Cooling Effectiveness

von Lee, Chien-Shing
Veröffentlicht in ASME Turbo Expo (2020 : Online) Proceedings of the ASME Turbo Expo 2020: Turbomachinery Technical Conference and Exposition - 2020 ; Volume 7, B (2020)

GT2022-82675 Computational and Experimental Study of Film-Cooling Effectiveness With and Without Downstream Vortex Generators

von Lee, Chien-Shing
Veröffentlicht in ASME Turbo Expo (67. : 2022 : Rotterdam) Proceedings of ASME Turbo Expo 2022: Turbomachinery Technical Conference and Exposition (GT 2022) ; Volume 6, A: Heat transfer: Combustors, film cooling (2022)