2020
DOI: 10.1016/j.jqsrt.2020.107082
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Effects of alumina particle clusters on UV radiation signature in the aircraft plume

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Cited by 9 publications
(4 citation statements)
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“…During the simulation, the aircraft's plume is modeled as a three-dimensional axisymmetric finite-length cylindrical model as shown in Figure 1. The distributions of the extinction coefficient, temperature, and chemiluminescence radiation emission coefficient within the plume region were obtained from references [7] and interpolated to achieve the threedimensional spatial distribution of the plume flow field [8] . The length of the plume model was selected to be 0.8m, with the cross-sectional radius of the plume model being 0.1m.…”
Section: Resultsmentioning
confidence: 99%
“…During the simulation, the aircraft's plume is modeled as a three-dimensional axisymmetric finite-length cylindrical model as shown in Figure 1. The distributions of the extinction coefficient, temperature, and chemiluminescence radiation emission coefficient within the plume region were obtained from references [7] and interpolated to achieve the threedimensional spatial distribution of the plume flow field [8] . The length of the plume model was selected to be 0.8m, with the cross-sectional radius of the plume model being 0.1m.…”
Section: Resultsmentioning
confidence: 99%
“…In the field of UV detection technology, Zhang et al 4 calculated the UV radiation of the tail flame based on the simulation results of the plume field of the aircraft and proposed a UV imaging detection scheme for the target tail flame.Huang et al 5 studied the mechanism of the UV radiation of the missile tail flame and calculated the UV radiation characteristics of the missile tail flame under the atmospheric background by using the Lowtran 7 software. As for the combination of UV and radar, Gao Fei et al 6 designed a UV multi-longitudinal mode high spectral resolution lidar system.…”
Section: Introductionmentioning
confidence: 99%
“…Missiles mainly propelled by solid or liquid fuels can produce UV radiation in the process of flying, originating from three sources: (i) the unburned solid fuel particles in the exhaust plume of the missiles during flight will mix with the air outside the engine and secondary combustion occurs, resulting in high temperature particle radiation. 5 (ii) The chemical luminescence caused by CO-O recombination will also be emitted during the secondary combustion of unburned fuel. 6 (iii) The skin of the missile rigging and tank emits UV radiation by friction with the atmosphere during the reentry segment.…”
Section: Introductionmentioning
confidence: 99%