International Journal of Aerospace Engineering / 2009 / Article / Fig 4

Research Article

Combined Magnetohydrodynamic and Geometric Optimization of a Hypersonic Inlet

Figure 4

Full inlet demonstrating initial conditions—Shock-canceled case.
793647.fig.004a
(a) Initial inlet configuration with shock canceling
793647.fig.004b
(b) Mach contours for the shock canceled configuration

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