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Abstract
The pulsed interaction of an ionized gas flow in a full-internal-compression diffuser with magnetic and electric fields has been experimentally studied. The interaction is determined by the shape of the electric current pulse between electrodes situated in the initial part of a hypersonic diffuser. It is established that, after termination of the current pulse, some characteristics of the shock wave front configuration in the gas flow exhibit relaxation with a significant delay to the unperturbed values.
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