The discussion centers on the construction of High-Pressure Turbine (HPT) blades and their cooling holes, specifically referencing the CFM56-5C engine. The user seeks assistance in finding simulation data regarding the source of cooling air for HPT blades, particularly how internal cooling utilizes High-Pressure Compressor (HPC) air. Participants clarify whether the user is looking for research facilities or academic papers on the topic.
PREREQUISITESAerospace engineers, turbine design specialists, and researchers in thermal management of turbine engines will benefit from this discussion.
Sorry, i have noted that there are cooling system in a particular HPT Blade design basically for CFM56-5C. Just wanted to know if someone could provide simulation in which where the cooling air came from (e.g internal cooling of HPT came from the HPC air and etc.billy_joule said:It's a little unclear what you are asking. Do you want to find turbine research facilities to perform your own experiments in or are you looking for papers on the subject?