Abstract:Utilizing gasoline as the fuel, air as oxidizer, a series of multi-cycle
detonation experiments was conducted to study thrust augmentation by
PDE-driven ejectors. The straight cylindrical ejectors with different inner
diameter, length and inlet geometry were designed. The effects of the axial
location of the ejectors relative to the end of the detonation tube, ejector
length-to-diameter ratio on thrust augmentation were investigated, with the
operating frequency of 25 Hz. A peak thrust augmen… Show more
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