论文信息 - Combustion Mechanism Downstream of a Cavity Flameholder Interacting with an Incident Shock Wave in Supersonic Flow - 字舞流文

Combustion Mechanism Downstream of a Cavity Flameholder Interacting with an Incident Shock Wave in Supersonic Flow

Taku Kudo | Hideaki Kobayashi | Akihiro Hayakawa | Yumi Ishimoto | Taku Kudo | A. Hayakawa | Hideaki Kobayashi | Y. Ishimoto

[1] Taku Kudo,et al. Effect of the incident shock wave interacting with transversal jet flow on the mixing and combustion , 2011 .

[2] Campbell D. Carter,et al. Stability limits of cavity-stabilized flames in supersonic flow , 2005 .

[3] Tarun Mathur,et al. Fundamental Studies of Cavity-Based Flameholder Concepts for Supersonic Combustors , 2001 .

[4] R. Yetter,et al. Flow reactor studies and kinetic modeling of the H2/O2 reaction , 1999 .

[5] Meng-Sing Liou,et al. A Flux Splitting Scheme with High-Resolution and Robustness for Discontinuities(Proceedings of the 12th NAL Symposium on Aircraft Computational Aerodynamics) , 1994 .