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旋流燃烧室内湍流燃烧速度场的实验研究 被引量:9

MEASUREMENTS OF THE VELOCITY FIELDS FOR TURBULENT COMBUSTION IN A SWIRL COMBUSTOR
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摘要 建立了采用分级进风方式的同轴射流旋流燃烧室实验装置,选用耐高温的氧化铝细粉作为示踪粒子,实现了用三维激光粒子动态分析仪(PDA)测量湍流旋流燃烧的热态瞬时速度场.在分级进风比率和旋流数不同的3组实验工况条件下,得到了气体时均轴向与切向速度、轴向与切向脉动速度均方根值和轴向-切向脉动速度二阶关联量的分布. A test facility for swirl combustor with coaxial jets and staged air injection was designed, fabricated, and set up. Fine alumina particles with high temperature endurance were chosen as seed particles in the tests. The instantaneous gas velocity fields of swirling turbulent combustion were measured by utilizing the Three-Dimension Laser Particle Dynamic Analyzer (PDA). Three cases of measurements were conducted. The distributions of the time-averaged gas axial and tangential velocities, the root mean square of fluctuating gas axial and tangential velocities, and the second-order correlation moment for the fluctuating gas axial and tangential velocities are obtained under different staged air injection ratios and swirl numbers. It is found that the gas axial velocity is relatively high in the central region of the combustor. The gas tangential velocity decays fast in the reacting flow. The turbulent exchange and transport are relatively strong in the central region due to the swirling and non-swirling jet interactions.
出处 《力学学报》 EI CSCD 北大核心 2003年第3期341-347,共7页 Chinese Journal of Theoretical and Applied Mechanics
基金 国家自然科学基金资助项目(59806006) 清华大学实验室开放基金资助项目
关键词 湍流旋流燃烧 PDA测量 燃烧实验 同轴射流 旋流燃烧室 swirling turbulent combustion, PDA measurement, combustion test, coaxial jets, swirl combustor
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参考文献5

  • 1Gouldin FC, Depsky JS, Lee SL. Velocity field characteristics of a swirling flow combustor. AIAA Journal, 1985, 23:95-102.
  • 2Brum RD, Samuelsen GS. Two-component laser anemometry measurements of non-reacting and reacting complex flows in a swirl-stabilized model combustor. Experimentsin Fluids, 1987, 5:95-102.
  • 3Charles RE, Samuelson GS. An experimental data base for the computational fluid dynamics of combustors. ASME Journal of Engineering for Gas Turbines and Power, 1989,111:11-14.
  • 4Hedman PO, Warren DL. Turbulent velocity and temperature measurements from a gas-fueled tecllnology combustor with a practical fuel injector. Combustion and Flame,1995, 100:185-192.
  • 5Anand MS, Takahashi F, Vangsness MD, et al. An experimental and computational study of swirling hydrogen jet diffusion flames. ASME Journal of Engineering for Gas Turbines and Power, 1997, 119:305-314.

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