AEDC team supports new measurement capability for turbine blades and vanes
This photo of a phosphor-coated dual vane section of a gas turbine engine, is positioned downstream of the AEDC J85 engine at the University of Tennessee Space Institute Propulsion Research Facility. The luminescence produced by the green laser beam and projected onto the phosphor-coated surface (left) is used to measure surface temperature. (Photo provided)
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