Combustion characteristics in a supersonic combustor with hydrogen injection upstream of cavity flameholder

By Hong-bo Wang, Zhenguo Wang, Mingbo Sun, Ning Qin. 2013

179 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Computational Mechanics

View Paper: https://www.semanticscholar.org/paper/e575e8e075b702d6b7dfbcc7fc0111921c2db83a

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. Ning Qin
2. Zhenguo Wang
3. Hong-bo Wang
4. Mingbo Sun

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

• Large eddy simulation of a hydrogen-fueled scramjet combustor with dual cavity (2015, methodology): “The experiments are carried out at National University of Defense Technology in a recently developed directconnected rig [4].”
• Review of cavity-stabilized combustion for scramjet applications (2014, background): “Close coupling of flow and combustion is important in supersonic reacting flows(98,99) especially for passive fuel injection where the jet-cavity interactions may introduce additional complexities.(15,23,100) As a result, care must be taken when applying the conclusions obtained in non-reacting flow”