Computational study of hypersonic rarefied gas flow over re-entry vehicles using the second-order Boltzmann-Curtiss constitutive model

The aerothermodynamics of re-entry vehicles vary significantly upon re-entry, descent, and landing, because of the drastic changes in atmospheric density and velocity. In highly rarefied regimes, the conventional Navier-Stokes-Fourier equations may not provide an accurate prediction of aerothermod...

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Main Authors: Chourushi, Tushar, Singh, Satyvir, Sreekala, Vishnu Asokakumar, Myong, Rho Shin
其他作者: School of Physical and Mathematical Sciences
格式: Journal Article
语言:English
出版: 2022
主题:
在线阅读:https://hdl.handle.net/10356/156103