Advanced Film Cooling Rig: Development and Test ResultsThe Advanced Film Cooling Rig (AFCR) test was a program to develop a thermal imaging camera system to measure the effectiveness of multihole film cooling. This system was used to evaluate low-thermal conductivity ceramic test panels incorporating a wide range of multihole cooling geometries. Tests were conducted with a mainstream flow of 600 F at Mach numbers of 0.37 and 1.57. Coolant flow was controlled to give a blowing parameter variation of up to 2.9. Data reduction techniques are given for camera calibration, rig temperature reflection correction, and deriving surface temperatures from video images. Results are presented in terms of overall and film cooling effectiveness distributions. A one-dimensional analysis of a unit film cooling hole was performed to generate film temperature.
Document ID
19970034938
Acquisition Source
Glenn Research Center
Document Type
Contractor Report (CR)
Authors
Reilly, R. S. (Pratt and Whitney Aircraft West Palm Beach, FL United States)
Date Acquired
August 17, 2013
Publication Date
August 1, 1997
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NAS 1.26:204136E-10851NASA-CR-204136GRC-E-DAA-TN42808Report Number: NAS 1.26:204136Report Number: E-10851Report Number: NASA-CR-204136Report Number: GRC-E-DAA-TN42808