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Features of the ignition kinetics of an H2/air mixture in the supersonic flow behind an inclined shock front are analyzed when asymmetric vibrations of a small amount (<1%) of O3 molecules specially introduced into the initial mixture are excited by 9.7 μm wavelength radiation. It is shown that this radiation leads to intensification of the chain reactions and makes it possible to organize combustion at small distances from the front (of the order of 1 m) of even relatively weak shocks at small values of the laser radiation energies absorbed by the gas. This method of initiating combustion in a supersonic flow is 10–100 times more efficient than the thermal method.__________Translated from Izvestiya Rossiiskoi Academii Nauk, Mekhanika Zhidkosti i Gaza, No. 2, 2005, pp. 157–167.Original Russian Text Copyright © 2005 by Lukhovitskii, Starik, and Titova. 相似文献
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This paper reports on two-dimensional numerical simulation of cellular detonation wave in a
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mixture with low initial pressure using a detailed chemical reaction model and high order WENO scheme. Before the final equilibrium structure is produced, a fairly regular but still non-equilibrium mode is observed during the early stage of structure formation process. The numerically tracked detonation cells show that the cell size always adapts to the channel height such that the cell ratio is fairly independent of the grid sizes and initial and boundary conditions. During the structural evolution in a detonation cell, even as the simulated detonation wave characteristics suggest the presence of an ordinary detonation, the evolving instantaneous detonation state indicates a mainly underdriven state. As a considerable region of the gas mixture in a cell is observed to be ignited by the incident wave and transverse wave, it is further suggested that these two said waves play an essential role in the detonation propagation.Received: 16 September 2003, Accepted: 14 June 2004, Published online: 20 August 2004[/PUBLISHED]PACS:
47.40.-x, 82.40.Fp, 82.33.Vx, 83.85.PtX.Y. Hu: Correspondence to Current address: Institut für Strömungsmechanik, Technische Universität Dresden, 01062 Dresden, Deutschland 相似文献
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Influence of multiwall carbon nanotube (MWCNT) dispersion on ignition of poly(dimethylsiloxane)–MWCNT composites
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Poly(dimethylsiloxane) (PDMS) filled with low contents of multiwall carbon nanotubes (MWCNT) was prepared using different ways to monitor the dispersion of MWCNT. The influence of the dispersion on thermal conductivity and transmittance was measured. High degree of transparence can be achieved with 0.02 phr of well dispersed MWCNT. Time‐to‐ignition (TTI) was also measured on 2‐ or 4‐mm‐thick specimens heated using radiative unidirectional source. Time‐to‐ignition was found to decrease with the incorporation of MWCNT because more heat is absorbed at the surface. Higher time‐to‐ignition was observed for partially translucent composites, due to different absorption in‐depth profiles. It can be assumed that time‐to‐ignition can be controlled by the dispersion of MWCNT into the polymeric matrix. Copyright © 2015 John Wiley & Sons, Ltd. 相似文献
35.
建立了再生喷射燃烧过程的多功能实验装置和瞬态参数测量系统。针对点火器参数对点火特性的影响规律进行了大量的实验研究,导出了点火器参数与点火特性之间的实用定量关系曲线。在此基础上,进行了相应的再生喷射燃烧过程实验,取得了较好地实验结果。研究表明:通过控制点火器参数以获得与再生喷射燃烧过程的匹配要求相适应的点火特性,对获得性能良好的燃烧过程具有重要意义。 相似文献
36.
碳氢燃料点火燃烧的简化化学反应动力学模型 总被引:3,自引:1,他引:3
基于``准稳态'方法建立了一套复杂化学反应动力学模型简化方法和相应的软件SPARCK.
并以3种典型的碳氢燃料------甲烷、乙烯和庚烷为研究对象,从甲烷点火燃烧的GRI2.11详
细基元反应动力学模型出发简化得出了包含14个组分10步总包反应形式的简化化学反应动
力学模型,从乙烯燃烧的51组分365详细基元反应模型出发简化得出了包含20个组分16
步总包反应形式的简化化学反应动力学模型,从庚烷点火燃烧的160组分1540详细基元反
应模型出发简化得出了包含26个组分22步总包反应形式的简化化学反应动力学模型. 通过
对典型激波管试验的结果对比可以看出:得到的简化反应动力学模型能较为有效地再现
详细基元反应模型的反应机理,具有较高的计算精度. 在工程计算中有较好的应用前景. 相似文献
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Osamu Moriue Masato Mikami Naoya Kojima Christian Eigenbrod 《Proceedings of the Combustion Institute》2005,30(2):1973-1980
Spontaneous ignition of single n-heptane droplets in a constant volume filled with air is numerically simulated with the spherical symmetry. The volume is closed against mass, species, and energy transfer. The numerical model is fully transient. It continues calculation even after the droplet has completely vaporized, and therefore can predict pre-vaporized ignition. Initial pressure and initial air temperature are fixed at 3 MPa and 773 K, respectively. The droplet is initially at room temperature, and its diameter is between 1 and 100 μm. When the overall equivalence ratio is fixed to be sufficiently large, there exists no ignition limit in terms of initial droplet diameter d0, and the ignition delay takes a minimum value at certain d0. In such a case, transition from the heterogeneous ignition to the homogeneous ignition with decreasing d0 is observed. When d0 is fixed to be so small that the ignition would not occur in an infinite volume of air, the ignition delay takes a minimum value at certain , which is less than unity. Two-stage ignition behavior is investigated with this model. Ignition delay of a cool flame has the dependence on d0 that is similar to that of ignition delay of a hot flame when is unity. When is almost zero, the ignition limit for cool flame in terms of d0 is not identified unlike that for hot flame. 相似文献
40.
To be able to meet the demands of low emissions and fuel consumption ofmodern combustion engines, new ways have to be found to control thecombustion. We use new sensors to measure the pressure in the combustionchamber and analyze this signal with a neural network in order to receiveseveral form factors which can be used to control the ignition timing. Theneural network is trained off line with measured data and used on line toderive the form factors. The proposed algorithm can be computed in real timeon conventional digital signal processors and adapted to new engines withvery little effort. 相似文献