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The new paradigm for describing nonequilibrium chemistry phenomena for hypersonics applications involves using ab initio potentials and detailed calculations of rate coefficients. We compare results of these calculations with shock tube experiments for rate coefficients for nitrogen dissociation.
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This page is a summary of: Comparison of Potential Energy Surface and Computed Rate Coefficients for N2 Dissociation, Journal of Thermophysics and Heat Transfer, October 2018, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.t5417.
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