Long description of figure 5

Illustration shows enlarged turbine airfoil assembly with cooling holes, two separate platforms, and vanes It also shows the entire configuration labeling the cooling air inlet, pyrometer access window, airflow, SiC/SiC transition duct, test section with turbine airfoil insert, water-cooled thermocouple probe, cooling air inlet, and the position of the turbine airfoil assembly.


previous page Return to article


Last updated: June 25, 2003


Responsible NASA Official: Gynelle.C.Steele@nasa.gov
216-433-8258

Point of contact for NASA Glenn's Research & Technology reports: Cynthia.L.Dreibelbis@nasa.gov
216-433-2912
SGT, Inc.

Web page curator: Nancy.L.Obryan@nasa.gov
216-433-5793
Wyle Information Systems, LLC

NASA Web Privacy Policy and Important Notices