pulse detonation engine (PDE) is a type of propulsion system that uses detonation waves to combust the fuel and oxidizer mixture.[1][2] The engine is pulsed because the mixture must be renewed in the combustion chamber between each detonation wave and the next. Theoretically, a PDE can operate from subsonic up to a hypersonic flight speed of roughly Mach 5. An ideal PDE design can have a thermodynamic efficiency higher than other designs like turbojets and turbofans because a detonation wave rapidly compresses the mixture and adds heat at constant volume. Consequently, moving parts like compressor spools are not necessarily required in the engine, which could significantly reduce overall weight and cost. PDEs have been considered for propulsion since 1940.[3] Key issues for further development include fast and efficient mixing of the fuel and oxidizer, the prevention of autoignition, and integration with an inlet and nozzle.
Editorial: Biosensors & Bioelectronics
Editorial: Biosensors & Bioelectronics
Editorial: Biosensors & Bioelectronics
Editorial: Biosensors & Bioelectronics
Review Article: Biosensors & Bioelectronics
Review Article: Biosensors & Bioelectronics
Editorial: Biosensors & Bioelectronics
Editorial: Biosensors & Bioelectronics
Research Article: Biosensors & Bioelectronics
Research Article: Biosensors & Bioelectronics
Keynote: Biosensors & Bioelectronics
Keynote: Biosensors & Bioelectronics
Accepted Abstracts: Biosensors & Bioelectronics
Accepted Abstracts: Biosensors & Bioelectronics
Scientific Tracks Abstracts: Journal of Civil and Environmental Engineering
Scientific Tracks Abstracts: Journal of Civil and Environmental Engineering
ScientificTracks Abstracts-Workshop: Journal of Material Sciences & Engineering
ScientificTracks Abstracts-Workshop: Journal of Material Sciences & Engineering
Accepted Abstracts: Journal of Material Sciences & Engineering
Accepted Abstracts: Journal of Material Sciences & Engineering
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