Abstract
Study of high enthalpy planetary entry vehicles demands a proper understanding of heating effects associated with thermal and chemical non-equilibrium phenomena, so that appropriate thermal protection systems can be designed.
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Srinath, S., Reddy, K.P.J. (2015). Experimental Measurement of Aerodynamic Heat Transfer due to Radiative Transmission in High Enthalpy Flow around a Re-entry Model. In: Bonazza, R., Ranjan, D. (eds) 29th International Symposium on Shock Waves 1. ISSW 2013. Springer, Cham. https://doi.org/10.1007/978-3-319-16835-7_100
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DOI: https://doi.org/10.1007/978-3-319-16835-7_100
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