Combustion oscillations in a scramjet engine combustor with transverse fuel injection

By Jeong-Yeol Choi, Fuhua Ma, Vigor Yang. 2005

162 citations recorded by the source corpus.

Subfields: Computational Mechanics

View Paper: https://www.semanticscholar.org/paper/b02bd3a01053e012a96e2c25766d33a7e6f57d54

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. Vigor Yang
5. Nana Zong
6. B. Chehroudi
7. Thierry Poinsot

Citations in the corpus

• Review of cavity-stabilized combustion for scramjet applications (2014, background): “High-frequency, strong pressure oscillations related to selfsustained cavity oscillations were observed in both non-reacting and reacting supersonic flows.(71,74,75) One of the possible mechanisms responsible for these combustion oscillations was found to be the unsteady flame spreading from the cav”
• Acoustic Characterization of an Ethylene-Fueled Scramjet Combustor with a Cavity Flameholder (2010, background): “[6] for a hydrogenfueled scramjet has clearly demonstrated such flow instability.”