Hi all,

Can anyone tell me where to find the data of any (existing & in use) turbine blade ie , geometry (including the location & coordinates of cooling holes), temperature/wall heat flux distribution. I need to solve a practical problem to test my unstructured mesh code. If anybody work on this & has results ... we can compare our results.

Thanks

Abhijeet

http://www.unibw-muenchen.de/campus/LRT12/

There are very complete investigations about cooling effects on blade performance (high pressure blade AGTB and low pressure blade T106). Of course, experimental conditions are not turbine operating conditions (for the AGTB blade, total inlet temperature is 300K). You have to e-mail the contact person to have a user ID and a password.

Good luck,

Nicola