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The use of liquid fuels such as kerosene is of interest for the Pulse Detonation Engine (PDE). In this context, a representative
gaseous mixture of the lighter products resulting from the decomposition of a kerosene of type JP-10 was studied. The detonability
limits of simple components (hydrogen, ethylene, propylene) and mixtures of these components were tested in a 50 mm diameter
and 2.5 m long detonation tube. This dimension is compatible with the applications of the aircraft industry and more particularly
the PDE. The influences of the nitrogen dilution, geometry of the DDT device (Schelkin spiral), ignition energy and initial
pressure were investigated.
This paper was based on work that was presented at the 19th International Colloquium on the Dynamics of Explosions and Reactive
Systems, Hakone, Japan, July 27 - August 1, 2003.
Communicated by J.E. Shepherd 相似文献
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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 of PDRE is a function of the nozzle contraction/expansion ratio and the operating frequency. The relationship between the nozzle contraction ratio and the operation frequency is obtained by introducing the duty ratio, by which the key problem in the theoretical design can be solved. Therefore, the performance of PDRE can be accessed to guide the preliminary shape design of nozzle conveniently and quickly. The higher the operating frequency of PDRE is, the smaller the nozzle contraction ratio should be. Besides, the lower the ambient pressure is, the larger the expansion ratio of the nozzle should be. When the ambient pressure is 1.013 × 105 Pa, the optimal expansion ratio will be less than 2.26.When the ambient pressure is reduced to vacuum, the extremum of the optimal thrust coefficient is 2.236 9, and the extremum of the specific impulse is 321.01 s. The results of the improved model are verified by numerical simulation. 相似文献