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Pulse Detonation Propulsion
SEMENOV INST OF CHEMICAL PHYSICS MOSCOW (RUSSIA)
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The objective of theoretical, computational and experimental studies outlined in this lecture note was to evaluate the design principles and propulsion performance of prospective air-breathing engines operating on pulse detonations of realistic hydrocarbon fuels with a realistic technique of detonation initiation via deflagration-to-detonation transition DDT.
APPROVED FOR PUBLIC RELEASE