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Advances in Pulsed and Continuous Detonation最新文献

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RESEARCH AND DEVELOPMENT OF ROTATING DETONATION ENGINE SYSTEM FOR THE SOUNDING ROCKET FLIGHT EXPERIMENT 探空火箭飞行试验用旋转爆轰发动机系统的研究与开发
Pub Date : 2019-07-31 DOI: 10.30826/icpcd201820
J. Kasahara, A. Kawasaki, K. Matsuoka, A. Matsuo, I. Funaki, D. Nakata, M. Uchiumi
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引用次数: 0
ANALYSIS OF ADVANCED TURBINE INTEGRATION WITH ROTATING DETONATION COMBUSTORS USING A TIME-ACCURATE REDUCED-ORDER MODEL 先进涡轮与旋转爆震燃烧室集成的时间精确降阶模型分析
Pub Date : 2019-07-31 DOI: 10.30826/icpcd201828
J. Braun, G. Paniagua
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引用次数: 0
ON THE UTILIZATION OF THE KINETIC ENERGY OF PULSED DETONATION PRODUCTS 论脉冲爆轰产物动能的利用
Pub Date : 2019-07-31 DOI: 10.30826/icpcd201827
S. Frolov, V. S. Smetanyuk, P. Gusev, A. Koval, S. A. Nabatnikov, Novel Physical Principles Ltd.
The possibility of utilizing the kinetic energy of detonation products by a pulse turbine of the simplest water-wheel-like design during the implementation of the Zel£dovich thermodynamic cycle with pulse detonation combustion of fuel is investigated computationally and experimentally. The coe©cients of utilization of the momentum and kinetic energy of detonation products in the pulse turbine with unoptimized mass and dimensions are found to be as low as 8%€16%. To improve the e©ciency of the pulse turbine, it is necessary to take measures for eliminating unnecesary re§ections of shock waves (SWs), to select the optimal mass and dimensions of the turbine rotor and the number of blades, to pro¦le the blades and to select the optimal angle of attack, to optimize the size of the lateral gap between the rotor and the housing, and to select the optimum location of the exhaust duct. It is expected that the e©ciency of a combined cycle including the optimized pulse turbine and conventional gas and/or steam turbines attached to the exhaust duct could be higher than the e©ciency of a conventional hybrid cycle by at most 9%.
本文从计算和实验两方面探讨了在燃料脉冲爆轰燃烧的泽尔多维奇热力学循环中,最简单的水轮式脉冲涡轮利用爆轰产物动能的可能性。未优化质量和尺寸的脉冲涡轮爆轰产物的动量和动能利用率低至8% ~ 16%。为了提高脉冲涡轮的效率,需要采取措施消除不必要的激波反射,选择涡轮转子的最佳质量和尺寸,选择叶片的最佳数量,选择叶片的最佳迎角,优化转子与机壳横向间隙的大小,选择排气管道的最佳位置。预计包括优化后的脉冲涡轮和附加在排气管道上的传统燃气轮机和/或蒸汽轮机在内的联合循环的e©效率比传统混合循环的e©效率最高可提高9%。
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引用次数: 0
ON THE DEPENDENCE OF REACTION RATE ON STRAIN RATE OF REACTING MEDIUM 反应速率与反应介质应变速率的关系
Pub Date : 2019-07-31 DOI: 10.30826/icpcd201804
V. Troflmov, V. Veretennikov, E. Petrov
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引用次数: 0
APPLICATION OF THE DETAILED REACTION MECHANISM OF FUEL OXIDATION FOR MODELING MULTISTAGE AUTOIGNITION IN DIESEL ENGINE 燃料氧化详细反应机理在柴油机多级自燃建模中的应用
Pub Date : 1900-01-01 DOI: 10.30826/icpcd201801
S. Sergeev, S. Frolov, V. Basevich, F. Frolov, B. Basara, P. Priesching
Three-dimensional (3D) numerical simulations of mixture formation, autoignition, and combustion processes in a cylinder of Diesel engine using the detailed reaction mechanism (DRM) of fuel oxidation (liquid n-tetradecane and liquid surrogate fuel containing 56%(wt.) n-hexadecane and 44%(wt.) toluene) are performed. Special attention is paid to the autoignition process. Calculations show that despite the high in-cylinder temperature before the start of fuel injection (∼ 1100 K), the autoignition of fuel spray has a staged nature with cool and blue §ames followed by hot explosion. The in§uence of the numerical time step and spatial resolution of the exothermic centers on the multistage autoignition is investigated. It has been established that for the correct modeling of the autoignition delay, both the integration time step and spatial resolution must be varied in such a way
利用燃料氧化(液体正十四烷和含56%正十六烷和44%甲苯的液体替代燃料)的详细反应机理(DRM),对柴油机汽缸内混合气形成、自燃和燃烧过程进行了三维(3D)数值模拟。特别注意的是自动点火过程。计算表明,尽管燃油喷射开始前的缸内温度很高(~ 1100k),但燃油喷雾的自燃具有分阶段的性质,先是冷爆,然后是热爆。研究了放热中心的数值时间步长和空间分辨率对多级自燃的影响。研究表明,为了正确地建立自燃延迟模型,积分时间步长和空间分辨率必须同时改变
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引用次数: 0
STEADILY-ROTATING, SEMICONFINED, OVERDRIVEN DETONATION: AN EXPERIMENTAL STUDY 稳定旋转、半精细、超驱动爆轰:实验研究
Pub Date : 1900-01-01 DOI: 10.30826/icpcd201822
C. Jourdain, V. Rodriguez, R. Zitoun, P. Vidal
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引用次数: 0
期刊
Advances in Pulsed and Continuous Detonation
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