Numerical investigation on the transverse jet into a supersonic crossflow with different pressure ratios
Author:
Affiliation:
1. Key Laboratory of Transient Physics, Nanjing University of Science and Technology, Nanjing, People’s Republic of China
2. School of Energy and Power Engineering, Nanjing University of Science and Technology, Nanjing, People’s Republic of China
Funder
National Natural Science Foundation of China
Publisher
Informa UK Limited
Link
https://www.tandfonline.com/doi/pdf/10.1080/19942060.2024.2354760
Reference44 articles.
1. Time evolution and mixing characteristics of hydrogen and ethylene transverse jets in supersonic crossflows
2. Effect of cavity geometry on fuel transport and mixing processes in a scramjet combustor
3. Existence of shocklets in a two-dimensional supersonic mixing layer and its influence on the flow structure
4. A prediction model of wall shear stress for ultra-high-pressure water-jet nozzle based on hybrid BP neural network
5. Scramjet Engines: The First Forty Years
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