We examine key issues that determine pulsed detonation engine (PDE) propulsive efficiency. Using Computational Fluid Dynamics methodology (CFD), we conducted performance analysis for the device for which we demonstrated multi-cycle operation experimentally. The analysis is focused on the effects of the non-ideal detonations on the propulsive efficiency. General questions of the methodology of nonsteady engine cycle analysis and performance evaluation are examined.
CITATION STYLE
Eidelman, S., Yang, X., & Lottati, I. (1995). Pulsed detonation engine: Key issues. In 31st Joint Propulsion Conference and Exhibit. American Institute of Aeronautics and Astronautics Inc, AIAA. https://doi.org/10.1007/978-94-011-5432-1_17
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