Correlation between Hypermixer and Fuel Injection Locations

Author:

Kim Chae-hyoung1,Jeung In-Seuck1,Choi Byungil2,Kouchi Toshinori2,Masuya Goro2

Affiliation:

1. Seoul National University

2. Tohoku University

Publisher

American Institute of Aeronautics and Astronautics

Cited by 5 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Design and Application of Filtered Rayleigh Scattering Experiments for Mixing Studies of New Strut Injectors for Scramjets;31st AIAA Aerodynamic Measurement Technology and Ground Testing Conference;2015-06-19

2. Stereoscopic particle image velocimetry measurements of supersonic, turbulent, and interacting streamwise vortices: challenges and application;Progress in Aerospace Sciences;2014-04

3. Planar Imaging Investigation of Supersonic Hypermixer Configurations;51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2013-01-05

4. Supersonic Combustion and Flame-Holding Characteristics of Pylon Injected Hydrogen in a Mach 2.4 High Enthalpy Flow;50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2012-01-09

5. Evolution of Large-Scale Structures Generated by a Strut Injector in a Mach 2.5 Flow;50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2012-01-09

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