air-he-44d_t.gif (32420 bytes)
air-he-58d_t.gif (17422 bytes)
air-he-77d_t.gif (20867 bytes)

A Planar Shock Wave Passes A Straight Gaseous Interface

Mach number=1.4

(1) Angle=44 degree

(2) Angle=58 degree

(3) Angle=77 degree

 

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cy_ball.gif (967 bytes)Details in Corresponding Paper