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- W2088897787 abstract "Pulse detonation engine (referred to as PDE) has many advantage about simple structure, high efficiency thermal <sup>[1]</sup> cycling etc. In the future, it can be widely used in unmanned aircraft, target drone, luring the plane, the imaginary target, target missiles, long-range missiles and other military targets. However, because the exhaust flame of PDE is complicated <sup>[2]</sup>, non-uniform temperature distribution and mutation in real time, its 3-D temperature distribution is difficult to be measured by normal way. As a result, PDE is used in the military project need to face many difficulties and challenges. In order to analyze and improve the working performance of PDE, deep research on the detonation combustion process is necessary. However, its performance characteristic which is in non-steady-state, as well as high temperature, high pressure, transient combustion characteristics put forward high demands about the flow field parameters measurement. In this paper, the PDE exhaust flames temperature field is reconstructed based on the theory of radiation thermometry <sup>[3]</sup> and Emission Spectral Tomography (referred to as EST) <sup>[4~6] </sup>which is one branch of Optical CT. It can monitor the detonation wave temperature distribution out of the exhaust flames at different moments, it also provides authentication for the numerical simulation which directs towards PDE work performance, and then it provides the basis for improving the structure of PDE." @default.
- W2088897787 created "2016-06-24" @default.
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- W2088897787 date "2010-05-13" @default.
- W2088897787 modified "2023-10-05" @default.
- W2088897787 title "Three-dimensional reconstruction method on the PDE exhaust plume flow flame temperature field" @default.
- W2088897787 doi "https://doi.org/10.1117/12.863853" @default.
- W2088897787 hasPublicationYear "2010" @default.
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