Characteristics of hydrogen jet combustion in a high-enthalpy supersonic crossflow
Author:
Affiliation:
1. Science and Technology on Scramjet Laboratory, National University of Defense Technology, Changsha 410073, China
2. Physikalisch-Technische Bundesanstalt (PTB), Bundesallee 100, 38116 Braunschweig, Germany
Funder
a fund for owner of outstanding doctoral dissertation from the Education Ministry of China
National Natural Science Foundation of China
Publisher
AIP Publishing
Subject
Condensed Matter Physics,Fluid Flow and Transfer Processes,Mechanics of Materials,Computational Mechanics,Mechanical Engineering
Link
http://aip.scitation.org/doi/pdf/10.1063/1.5084751
Reference49 articles.
1. Advances and challenges in modeling high-speed turbulent combustion in propulsion systems
2. High-fidelity resolution of the characteristic structures of a supersonic hydrogen jet flame with heated co-flow air
3. Raman measurement of mixing and finite-rate chemistry in a supersonic hydrogen-air diffusion flame
4. An explicit reduced mechanism for H2–air combustion
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