Numerical study on supersonic combustion with cavity-based fuel injection

By K. Kim, S. Baek, C. Han. 2004

249 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Computational Mechanics

View Paper: https://www.semanticscholar.org/paper/ec16829e2106b8478ca70296f641e53c8f4a6139

How researchers see this paper

The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.

In Aerospace Engineering

1. Wei Huang
2. Li Yan
3. Zhenguo Wang
4. Ning Qin
5. Hong-bo Wang
6. Mingbo Sun
7. Shibin Li

In Computational Mechanics

1. Wei Huang
2. Li Yan
3. Zhenguo Wang
4. Hong-bo Wang
5. Mingbo Sun
6. Ning Qin
7. Shibin Li
8. Christian B. Allen

Citations in the corpus

• Large eddy simulation of a hydrogen-fueled scramjet combustor with dual cavity (2015, methodology): “When used as an integrated fuel injection/flameholding approach [2], cavity flameholders have become even more attractive in supersonic combustors and received more and more attention [3–14].”
• Performance evaluation and parametric analysis on cantilevered ramp injector in supersonic flows (2013, background): “At the outflow, all the physical variables are extrapolated from the internal cells due to the flow being supersonic [20].”
• Influences of the turbulence model and the slot width on the transverse slot injection flow field in supersonic flows (2012, background): “At the outflow, all the physical variables are extrapolated from the internal cells due to the flow being supersonic [24,25].”