Combustion characteristics of a dual-mode scramjet combustor with cavity flameholder

By D. Micka, J. Driscoll. 2009

445 citations recorded by the source corpus.

Subfields: Computational Mechanics

View Paper: https://www.semanticscholar.org/paper/d75d22486c1b1e7254e07d391924c928194c6043

How researchers see this paper

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

In Computational Mechanics

1. Hong-bo Wang
2. Mingbo Sun
3. Zhenguo Wang
4. Ning Qin
5. Christian B. Allen
6. Thomas C. S. Rendall

Citations in the corpus

• Review of cavity-stabilized combustion for scramjet applications (2014, background): “Average combustion luminosity images for the two stabilization modes.(11) (a) Cavity stabilized combustion.”
• 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].”