Interactions of a plasma and an incoming flow at Mach 3
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چکیده
A mechanical spike is a device used to mechanically act on the bow shock ahead of an airplane in supersonic ight. This action results in improved ight conditions. We will investigate here the e ects of the axial generation of a two-hundred-micrometer width cylindrical plasma ahead a quasi-realistic nose pro le of centimeter width. The device is named plasma spike by analogy to the above-cited mechanical device. This plasma spike is a source of both momentum and energy for the neighboring uid.
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تاریخ انتشار 2010