Research Article

Magnetogasdynamic Shock Waves in a Rotating Gas with Exponentially Varying Density

Figure 2

Variation of reduced magnetic field in the region behind the shock front for 𝛾 = 1 . 4 . ( 1 )    𝑀 𝐴 2 = 0.05, 𝑡 / 𝑡 0 = 2; ( 2 )    𝑀 𝐴 2 = 0.1, 𝑡 / 𝑡 0 = 2; ( 3 )    𝑀 𝐴 2 = 0.05, 𝑡 / 𝑡 0 = 5; ( 4 )    𝑀 𝐴 2 = 0.1, 𝑡 / 𝑡 0 = 5.
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