航天推进技术研究院主办
Wu Baoyuan.Numerical investigation of supersonic combustor with cavity flameholder[J].Journal of Rocket Propulsion,2005,31(04):26-29.
带不同长度凹腔超声速燃烧数值研究
- Title:
- Numerical investigation of supersonic combustor with cavity flameholder
- 分类号:
- V434
- 文献标志码:
- A
- 摘要:
- 对带不同长深比凹腔的燃烧室三维燃烧流场进行数值模拟,研究了燃烧室流场结构。结果表明:液体碳氢燃料穿透深度较小;凹腔长深比对燃烧效率、总压损失影响较小,对燃烧室阻力影响显著。
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