Aerospace Science and Technology
 2023
DOI: 10.1016/j.ast.2023.108471
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Quantitative analysis of enhanced mixing and combustion by lobed mixer in a ramjet engine: Study using hyperbolic Lagrangian coherent structures

Lin Sun
1
,
Fang Bian
2
,
Xinying Lei
3
et al.
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Cited by 5 publications
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References 51 publications
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Effect of synergistic impact gas injection device on secondary combustion in boron-based ducted rockets

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Applied Thermal Engineering
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Numerical investigation of the distributed combustion in the thermal choked solid fuel combined cycle engine

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Fluid dynamic analysis and lift enhancement of material transport and mixing around airfoil through Lagrangian coherent structures

Zhang,
Cao,
Liu
2023
Results in Engineering
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