Abstract
The flowfield analysis around a model of space plane traveling at Mach 10 has been carried out utilizing an Electrical Discharge Method and a Finite Element Method scheme. In this study, the experiments and the numerical simulations were carried out under the conditions the angle of attack were 0 and 10 deg. Furthermore, the experimental results were compared with the numerical ones. In these comparisons, it was found that they were relatively in good agreement.
