Measurements of turbine blade temperature in an operating aero engine using thermographic phosphors
Author:
Funder
Air Force SBIR Program
Publisher
IOP Publishing
Subject
Applied Mathematics,Instrumentation,Engineering (miscellaneous)
Link
http://iopscience.iop.org/article/10.1088/1361-6501/ab4c20/pdf
Reference23 articles.
1. Gas Turbine Technology Evolution: A Designers Perspective
2. An overview of the measurement errors associated with gas turbine aeroengine pyrometer systems
3. Phosphor thermometry in an electron beam physical vapour deposition produced thermal barrier coating doped with dysprosium
4. Depth-penetrating temperature measurements of thermal barrier coatings incorporating thermographic phosphors
5. Non-contact sensing of TBC/BC interface temperature in a thermal gradient
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