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This paper develops a systematic approach for correcting shock-layer radiative heating simulations based on shock-tube measurements. This approach improves on previous techniques by being applicable to simulations away from the stagnation point and non-optically-thin conditions.
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This page is a summary of: Evaluating Shock-Tube Informed Biases for Shock-Layer Radiative Heating Simulations, Journal of Thermophysics and Heat Transfer, November 2020, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.t6174.
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