Enhancement and Control of Deflagration to Detonation Transition ( DDT ) in binary fuels C 3 H 8 − H 2 / air Mixtures : Application to Propulsion

Abstract

The Deflagration to Detonation Transition (DDT) that follows the flame acceleration has been investigated for different purposes, namely for safety concerns and for rapid transition in detonation-assisted propulsion systems. Beside its use in rocket propulsion, hydrogen is more and more regarded as an appropriate candidate for propulsive systems. Yet it is… (More)

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