期刊:Journal of Thermophysics and Heat Transfer [American Institute of Aeronautics and Astronautics] 日期:2001-04-01卷期号:15 (2): 148-156被引量:89
标识
DOI:10.2514/2.6603
摘要
A new transport coefficient model based on the first approximation of the Chapman-Cowling theory is implemented into the URANUS nonequilibrium NavierStokes Code in order to predict re-entry flows more accurately. The new model is compared to the widely used, simplified model of Gupta and Yos. The simplifications used to obtain the latter model are described in detail. The transport coefficients computed with both methods differ by up to a factor of two in the case of partially ionized air under equilibrium conditions. Therefore, the new model allows a more accurate description of the thermo-chemical relaxation in the shock region of significantly ionized, high-temperature flows. The differences in surface heat fluxes between the new model and the model of Yos and Gupta are smaller than 4%.