International Journal of Aerospace Engineering / 2009 / Article / Tab 1

Research Article

Combined Magnetohydrodynamic and Geometric Optimization of a Hypersonic Inlet

Table 1

Shock-canceled inlet flow conditions.

Region Mach number Flow angle

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

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