Effect of Flame-Holding Cavities on Supersonic-Combustion Performance

By K. Yu, K. Wilson, K. Schadow. 2001

147 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Computational Mechanics

View Paper: https://www.semanticscholar.org/paper/1abe9ada8d5a72b49d4db80de3e7e028e964ca2c

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

In Computational Mechanics

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

Citations in the corpus

• Numerical study on supersonic combustion with cavity-based fuel injection (2004, background): “Particularly, the numerical analysis of the fuel injection system accompanied by the cavity is rarely studied while it is only recent that its experimental work has been in progress [10,11].”
• Review of cavity-stabilized combustion for scramjet applications (2014, background): “and Yu et al.(64) stated that the inclined, stable cavities were preferred for flameholding, while Rasmussen et al.”
• Large eddy simulation of a hydrogen-fueled scramjet combustor with dual cavity (2015, background): “Under certain conditions, however, a single cavity may not be able to robustly stabilize the combustion, where multiple cavities could be used [16–21].”