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The focus of this paper is to provide a deeper understanding of the flow physics responsible for establishing the convective heat transfer on the sensor surface of vented-shield style total temperature probes upstream of the shield discharge ports/vents, where significant forced convection exists.

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This page is a summary of: Aerodynamic Analysis of Total Temperature Probe Thermal Performance Using Conjugate Heat Transfer, Journal of Thermophysics and Heat Transfer, July 2019, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.t5635.
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