Radiation equilibrium temperature calculation method considering slip correction
A technology of radiation balance and calculation method, applied in the directions of calculation, computer-aided design, design optimization/simulation, etc., can solve the problems of calculation failure, violent fluctuation of wall heat flow, and sliding temperature fluctuation, and achieve the effect of avoiding error iterative feedback amplification
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[0083] Example 1: Numerical simulation of the non-equilibrium rarefied slip flow and surface radiation equilibrium coupling of the reflector. Returner looks like figure 2 As shown, the calculation and simulation state is a flight altitude of 85km and an incoming flow velocity of 7600.0m / s. The high-temperature gas model is a 5-component air chemical reaction Park model and a single temperature model, and the slip model is a classic Maxwell slip model; the aircraft surface is completely catalyzed (FCW) and completely non-catalyzed (NCW).
[0084] image 3 The calculation result and literature (Votta R, Schettino A, Ranuzzi G, Borrelli S, Hypersonic low-density aerothermo-dynamics of orion-like exploration vehicle[J].Journal of Spacecraft and Rockets, 2009) of the present invention are given. , 4(46):781~787). It can be seen that the heat flow results are closer to the DSMC results.
[0085] Figure 4 The distribution of wall surface radiation equilibrium temperature and w...
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