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Empirical freestream characterization of high-enthalpy hypersonic ground facilities is critical to improving the certainty of inferred freestream conditions, which has propagating impacts on dependent flow model studies. This work represents a first step towards obtaining a better picture of the freestream conditions in the T5 Reflected Shock Tunnel at Caltech.

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This page is a summary of: Measurements of Reflected Shock Tunnel Freestream Nitric Oxide Temperatures and Partial Pressure, AIAA Journal, December 2021, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j060596.
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