Numerical simulation for aerodynamic heating and opposing jet thermal protection

Abstract

Based on the theory and semi-empirical formulas, the surface heating flux of warhead at zero attack angle under aerodynamic heating is calculated by using reference enthalpy method, and the equilibrium curves of temperature for radiation of wall are obtained, by which the anti-thermal effects of blunt leading edge is proved in this paper. At the same time… (More)

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Cite this paper

@article{Hongqing2008NumericalSF, title={Numerical simulation for aerodynamic heating and opposing jet thermal protection}, author={Lv Hongqing and Wang Zhenqing and Jin Chengbin and Zhang Cuie and Wang Yongjun}, journal={2008 2nd International Symposium on Systems and Control in Aerospace and Astronautics}, year={2008}, pages={1-5} }