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- W2356800858 abstract "For a underwater high speed aircraft-purposed magnesium-based hydroreactive metal fuel ramjet,set were fuels mixed in three component mass proportions and in conjunction with the thermal calculation and two-dimensional axis-symmetrical numerical simulation,studied were its operating characteristics.In this connection,the vortexes observed at both inlets foreshow that during the fuel combustion process,it is possible to result in a thermoacoustic oscillation.Within the effective ranges of water/fuel ratio specific to the ramjet burning three kinds of fuel respectively,the numerical simulation results show that the distribution of water/fuel ratios in two times will directly influence the combustion stability inside the engine.To increase the total water/fuel ratio will produce a maximal specific impulse and in the meantime,the thermal efficiency and the propulsion efficiency will increase and decrease respectively in a monotonous way.In addition,both numerical simulation and thermal calculation result indicate that to increase the megnesium content in the fuel will help increase the specific impulse and thermal efficiency of the engine.The law and characteristics governing the change of such operating characteristics of the engine as combustion characteristics,specific impulse and efficiency etc.can offer guide for optimizing overall structure and performance of an engine and at the same time,predict the intrinsic thermoacoustic oscillation characteristics of an engine so as to design corresponding control tactics." @default.
- W2356800858 created "2016-06-24" @default.
- W2356800858 creator A5056841329 @default.
- W2356800858 date "2012-01-01" @default.
- W2356800858 modified "2023-09-23" @default.
- W2356800858 title "Operating Characteristics of a Magnesium-based Hydroreactive Metal Fuel Ramjet" @default.
- W2356800858 hasPublicationYear "2012" @default.
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