The Effect of Interaction of Shock Waves with Boundary Layers to The Cold Internal Flow Field of A Dual-Combustor Scramjet Model

Zhang Shudao; Han Zhaoyuan; Xu Shengli; Situ Ming

doi:10.3969/j.issn.1672-9897.1999.02.003

Zhang Shudao, Han Zhaoyuan, Xu Shengli, Situ Ming. The Effect of Interaction of Shock Waves with Boundary Layers to The Cold Internal Flow Field of A Dual-Combustor Scramjet Model[J]. Journal of Experiments in Fluid Mechanics, 1999, 13(2): 16-21. DOI: 10.3969/j.issn.1672-9897.1999.02.003

Citation:

Zhang Shudao, Han Zhaoyuan, Xu Shengli, Situ Ming. The Effect of Interaction of Shock Waves with Boundary Layers to The Cold Internal Flow Field of A Dual-Combustor Scramjet Model[J]. Journal of Experiments in Fluid Mechanics, 1999, 13(2): 16-21. DOI: 10.3969/j.issn.1672-9897.1999.02.003

Citation:

Zhang Shudao, Han Zhaoyuan, Xu Shengli, Situ Ming. The Effect of Interaction of Shock Waves with Boundary Layers to The Cold Internal Flow Field of A Dual-Combustor Scramjet Model[J]. Journal of Experiments in Fluid Mechanics, 1999, 13(2): 16-21. DOI: 10.3969/j.issn.1672-9897.1999.02.003

The Effect of Interaction of Shock Waves with Boundary Layers to The Cold Internal Flow Field of A Dual-Combustor Scramjet Model

Graphical Abstract

Abstract

FullText(HTML)

References (0)

The Effect of Interaction of Shock Waves with Boundary Layers to The Cold Internal Flow Field of A Dual-Combustor Scramjet Model

Catalog

Export File

Citation

Format

Content