凹腔布置方案对气化煤油超声速燃烧特性的影响

针对两种凹腔布置方案，模拟马赫数6.0的来流条件，采用气化RP-3开展了一系列直连式燃烧试验。依据燃烧流场的可见光图像、燃烧室壁面静压分布和推力增益，对比分析了凹腔布置方案对气化煤油超声速燃烧特性的影响。结果表明，凹腔布置方案和当量比对燃烧室内的火焰分布、燃料的释热特性和发动机燃烧性能有显著影响。并联凹腔的火焰与释热主要集中在凹腔附近，燃料比冲对当量比不敏感；单凹腔的火焰与释热分布更加分散，燃料比冲随当量比的增加而提高。
Considering the two different cavity arrangement schemes, a series of direct-connected combustion tests were conducted with vaporized RP-3 under the simulated Mach 6.0 flight condition. Effects of cavity arrangement on characteristics of supersonic combustion of vaporized kerosene were investigated by comparing with the high-speed flame luminosity images, static pressure distributions along the combustor wall, and the thrust increments. The results show that the cavity arrangement and equivalence ratios affect the flame distribution, the heat release characteristic and the combustor performance significantly. For the parallel-cavity-equipped combustor, the flame distribution and heat release are concentrated near cavities, and the fuel specific impulse shows low sensitivity to the equivalence ratio. While the single-cavity-equipped combustor has a dispersive flame distribution and heat release, and the fuel specific impulse increases with the equivalence ratio.