Progress in Propulsion Physics 2009
DOI: 10.1051/eucass/200901321
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Detonation initiation techniques for pulse detonation propulsion

Abstract: The paper outlines recent e¨orts of the research team directed by the author on the development of e©cient means for reducing the de §agration-to-detonation transition (DDT) run-up distance and time for liquidfueled air-breathing pulse detonation engine (PDE) applications. The main objective of the studies was to ensure fast DDT in a PDE tube at the lowest possible ignition energy, at the shortest distance, with the lowest pressure loss, and using aviation kerosene TS-1 (Russian analogue of JetA) as fuel and a… Show more

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Cited by 7 publications
(1 citation statement)
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“…A detonation wave can be obtained by direct-initiation or deflagration-to-detonation transition (DDT) processes. DDT length and time are crucial parameters for PDE applications [4] and safety. Several physical and chemical factors influence the DDT parameters [5], one of the most important being the mixture detonability.…”
Section: Introductionmentioning
confidence: 99%
“…A detonation wave can be obtained by direct-initiation or deflagration-to-detonation transition (DDT) processes. DDT length and time are crucial parameters for PDE applications [4] and safety. Several physical and chemical factors influence the DDT parameters [5], one of the most important being the mixture detonability.…”
Section: Introductionmentioning
confidence: 99%