Combined Magnetohydrodynamic and Geometric Optimization of a Hypersonic Inlet

Table 1

Shock-canceled inlet flow conditions.

Region	Mach number	Flow angle	𝑃𝑡𝑖/𝑃𝑡𝑗	𝑃𝑡/𝑃𝑡∞
1	14.000	0.0	1	1
2	12.107	2.882	0.927	0.927
3	8.953	9.342	0.669	0.620
4	6.385	0.0	0.626	0.388