Heat and Radiative Fluxes in Strongly Nonequilibrium Flows Behind Shock Waves
Author:
Publisher
Pleiades Publishing Ltd
Subject
General Mathematics
Link
https://link.springer.com/content/pdf/10.1134/S1063454122040094.pdf
Reference21 articles.
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2. D. L. Cauchon, Radiative Heating Results from Fire II Flight Experiment at a Reentry Velocity of 11.4 km/s, NASA TM X-1402 (1967).
3. C. O. Johnston, B. R. Hollis, and K. Sutton, “Nonequilibrium stagnation-line radiative heating for Fire II,” J. Spacecr. Rockets 45, 1185–1195 (2008).
4. M. Panesi, T. E. Magin, A. Bourdon, A. Bultel, and O. Chazot, “Fire II flight experiment analysis by means of a collisional-radiative model,” J. Thermophys. Heat Transfer 23, 236–248 (2009).
5. S. T. Surzhikov, “Radiative gas dynamics of the Fire-II superorbital space vehicle,” Tech. Phys. 61, 349–359 (2016). https://doi.org/10.1134/S1063784216030208
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1. Scientific School of Nonequilibrium Aeromechanics at St. Petersburg State University;Vestnik St. Petersburg University, Mathematics;2023-09
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