134
P. Liu
Fig. 2.69 Oblique shock waves passing by a supersonic flow around the leading
edge
that the parameters such as velocity change continuously in the shock
wave, as shown in Fig. 2.71. The change in velocity from V 1 at the
front to V 2 at the back is a gradual process, so the shock thickness
cannot be clearly defined. Generally, the tangent of the curve is made
at the inflection point of the v-x curve, and the distance between the
intersection of the curve and the horizontal line with V 1 and V 2 as
constant values is the shock thickness.
P. Liu
Fig. 2.69 Oblique shock waves passing by a supersonic flow around the leading
edge
that the parameters such as velocity change continuously in the shock
wave, as shown in Fig. 2.71. The change in velocity from V 1 at the
front to V 2 at the back is a gradual process, so the shock thickness
cannot be clearly defined. Generally, the tangent of the curve is made
at the inflection point of the v-x curve, and the distance between the
intersection of the curve and the horizontal line with V 1 and V 2 as
constant values is the shock thickness.