DSMC simulation of Rarefied Hypersonic flows over wall mounted geometries
Author:
Affiliation:
1. Birla Institute of Technology & Science Pilani
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2023-3059
Reference34 articles.
1. Guo G and Luo Q. "Flowfield structure characteristics of the hypersonic flow over a cavity: from the continuum to the transition flowregimes". ActaAstronaut 2019;161:87-100. https://doi.org/10.1016/j.actaastro.2019.05.023
2. W. Zhang, Z. Zhang, X. Wang, T. Su, S. Zhang, "Hypersonic nonequilibrium flow simulations of a hemispherical nose with acounterflowing jet", ActaAstronautica.165 (2019)388-400. https://doi.org/10.1016/j.actaastro.2019.09.014
3. S. Kumar, S. Vengadesan," The effect of fin oscillation in heat transfer enhancement in separated flow over a backward facing step", Int. J.Heat MassTran. 128 (Jan.2019) 954-963. http://dx.doi.org/10.1016/j.ijheatmasstransfer.2018.09.001
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