An improved constant volume cycle model for performance analysis and shape design of PDRE nozzle
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DOI: 10.1007/s10483-018-2294-6
Abstract: An improved constant volume cycle (CVC) model is developed to analyze the nozzle effects on the thrust and specific impulse of pulse detonation rocket engine (PDRE). Theoretically, this model shows that the thrust coefficient/specific impulse… read more here.
Keywords: pdre; ratio; model; constant volume ... See more keywords