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    Please use this identifier to cite or link to this item: https://ir.fy.edu.tw:8080/ir/handle/987654321/10027

    Title: Ignition and Combustion Study of JP-8 Fuel in a Supersonic Flowfield
    Authors: Char,J. M.;Liou,W. J.;Yeh,J. H.;Chiu, C. L.
    Contributors: 輔英科技大學 環境工程與科學系
    Keywords: JP-8 fuel;Droplet ignition;Detonation
    Date: 1996-06
    Issue Date: 2010-11-16 16:30:24 (UTC+8)
    Abstract: The ignition and combustion process of fuels in a supersonic combustion chamber plays an important role in the design of hypersonic propulsion system. However, it is a quite complicated process, due to the large variation of inlet air velocity, temperature, oxygen concentration, and shocks in the supersonic combustion chamber. The purpose of this paper is to observe the ignition delay and combustion phenomenon of the JP-8 fuel droplets in a supersonic flowfield experimentally. A shock tube is used as a basic test facility to create a high-speed and high-temperature flowfield as a supersonic combustor. In the experiments, several test parameters are controlled, such as shock velocity, gas temperature, fuel droplet size and distance, initial fuel temperature, and oxygen concentration, etc. The test results show the influence of these parameters on ignition delay, ignition limitation, and detonation. The most important factor in the experiment is the initial fuel temperature effect, which is influenced by the altitude variation during a flight.
    Relation: Shock Waves,Volume 6, Number 5, p. 259-266
    Appears in Collections:[環境工程與科學系] 期刊論文

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