NASA NTRS · 19860002032
Dynamic gas temperature measurement system
Abstract
A gas temperature measurement system with compensated frequency response of 1 KHz and capability to operate in the exhaust of a gas turbine combustor was developed. Environmental guidelines for this measurement are presented, followed by a preliminary design of the selected measurement method. Transient thermal conduction effects were identified as important; a preliminary finite-element conduction model quantified the errors expected by neglecting conduction. A compensation method was developed to account for effects of conduction and convection. This method was verified in analog electrical simulations, and used to compensate dynamic temperature data from a laboratory combustor and a gas turbine engine. Detailed data compensations are presented. Analysis of error sources in the method were done to derive confidence levels for the compensated data.
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Elmore, D. L., Robinson, W. W., Watkins, W. B.. 1983-10-01. Dynamic gas temperature measurement system. https://ntrs.nasa.gov/citations/19860002032
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