期刊文献+

抛物面聚焦激波点火研究

Ignition investigation by paraboloid focusing shock wave
下载PDF
导出
摘要 为了研究物理破裂诱导火灾爆炸过程中的点火机理和改进超燃、爆震燃烧中的点火技术,将乙炔/空气可燃混合气体在59mm×59mm方形激波管内由抛物面聚焦激波进行点火实验。采用高速摄影技术对入射激波经过抛物面反射和聚焦的过程进行跟踪,得到反射激波聚焦的阴影图片以及聚焦点火的纹影照片。实验结果显示:当乙炔与空气的混合比处于理论化学当量比时,马赫数为2.1的聚焦激波能够引燃乙炔/空气的混合气体。火焰由抛物面反射后聚焦所形成的气体动力学焦点产生,且沿抛物面传播的速度最快。 To study the mechanism of ignition in the fire explosion process induced by physical rupture and improve the ignition technology in supersonic combustion or detonation combustion,the acetylene/air combustible gas mixture is ignited in a 59 mm×59 mm rectangular cross section shock tube induced by paraboloid focusing shock waves.The high-speed photography technology is applied to observe the process of the incident shock wave focusing and reflecting by the paraboloid.Shaded pictures of reflected shock wave focusing and schlieren photographs of focusing ignition are obtained.The results show that the combustible mixture of acetylene/air can be ignited by the focusing shock wave(Ma=2.1),if the acetylene/air blended near the theoretical chemical stoichiometric ratio.The flame is generated at the gas dynamics focus formed by the paraboloid reflection and focusing,and the spread speed of the flame is the fastest along the paraboloid.
出处 《南京理工大学学报》 EI CAS CSCD 北大核心 2013年第3期427-430,共4页 Journal of Nanjing University of Science and Technology
基金 国家自然科学基金(10472047)
关键词 抛物面聚焦 激波 点火 乙炔 空气 paraboloid focusing shock waves ignition acetylene air
  • 相关文献

参考文献7

二级参考文献50

  • 1李辉煌,杨基明,徐立功.脉冲爆震发动机喷管流动的数值模拟[J].推进技术,2004,25(6):553-556. 被引量:12
  • 2王昌建,徐胜利.直管内胞格爆轰的基元反应数值研究[J].爆炸与冲击,2005,25(5):405-416. 被引量:14
  • 3董刚,唐敖,叶经方,范宝春.激波聚焦诱导点火和爆轰的数值研究[J].爆炸与冲击,2005,25(5):437-444. 被引量:8
  • 4滕宏辉,张德良,李辉煌,姜宗林.用环形激波聚焦实现爆轰波直接起爆的数值模拟[J].爆炸与冲击,2005,25(6):512-518. 被引量:14
  • 5Sislian J P, Schirmer H, Dudebout R, et al. Propulsive performance of hypersonic oblique detonation wave and shock-induced combustion ramjets. J Propul Power, 2001, 17(3): 599-604.
  • 6Couture D, Dechamplain A, Stowe R A, et al. Comparison of scramjet and shcramjet propulsion for a hypersonic waverider configuration. AIAA Paper 2008-5171, 2008.
  • 7Wang Y W, Sislian J P. Numerical investigation of methane and air mixing in a shcramjet inlet. AIAA Paper 2008-2533, 2008.
  • 8Dudebout R, Sislian J P, Oppitz R. Numerical simulation of hypersonic shock-induced combustion ramjets. J Propul Power, 1998, 14(6): 869--879.
  • 9Schwartzentruber T E, Sislian J P, Parent B. Suppression of premature ignition in the premixed inlet flow of a shcramjet. J Propul Power, 2005, 21(1): 87-94.
  • 10Sislian J P, Schumacher J. A comparative study of hypersonic fuel/air mixing enhancement by ramp and cantilevered ramp injectors. AIAA Paper 99-4873, 1999.

共引文献22

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部