期刊文献+
共找到4篇文章
< 1 >
每页显示 20 50 100
固体火箭发动机冷气冲击瞬态内流场分析 被引量:3
1
作者 何凡 余陵 +1 位作者 蔡文祥 杨玲 《固体火箭技术》 EI CAS CSCD 北大核心 2015年第1期67-72,共6页
运用高压氮气冲击固体火箭发动机来模拟在发动机点火时产生的高压峰值对药柱及发动机壁面的冲击,测量出发动机头部、中部、尾部的压力分布,对固体火箭发动机冷气冲击试验过程进行模拟。应用(fluent)流体计算软件,对瞬时内流场进行了二... 运用高压氮气冲击固体火箭发动机来模拟在发动机点火时产生的高压峰值对药柱及发动机壁面的冲击,测量出发动机头部、中部、尾部的压力分布,对固体火箭发动机冷气冲击试验过程进行模拟。应用(fluent)流体计算软件,对瞬时内流场进行了二维轴对称非定常数值分析。研究结果表明,所模拟的3个测量点压力-时间曲线与试验曲线吻合较好,药柱头部位置及内端面受冲击力较大,易造成结构完整性破坏,进一步证明试验能够较好的模拟真实点火峰压对发动机及药柱造成的影响,为发动机点火设计及试验提供有力的参考。 展开更多
关键词 固体火箭发动机 冷气冲击 数值模拟 内流场
下载PDF
固体火箭发动机冷气冲击过程数值分析 被引量:2
2
作者 杨辰 余陵 +1 位作者 蔡文祥 祁斌 《四川兵工学报》 CAS 2015年第11期141-144,共4页
使用工业氮气冲击固体火箭发动机药柱以模拟发动机点火瞬时产生的高压峰值对发动机壁面的压力冲击,分析模拟固体火箭发动机工作中的压力分布,对冷气冲击试验过程进行数值模拟;运用流体计算软件Fluent,对瞬时内流场进行二维轴对称非定常... 使用工业氮气冲击固体火箭发动机药柱以模拟发动机点火瞬时产生的高压峰值对发动机壁面的压力冲击,分析模拟固体火箭发动机工作中的压力分布,对冷气冲击试验过程进行数值模拟;运用流体计算软件Fluent,对瞬时内流场进行二维轴对称非定常数值分析;研究分析结果表明:药柱头部位置受冲击力较大,容易产生结构完整性破坏,进一步验证发动机冷气冲击试验能够较好的模拟真实情况下发动机及药柱受到的影响,从而为发动机点火设计提供参考。 展开更多
关键词 冷气冲击 固体火箭发动机 数值模拟
下载PDF
Fracture evolution in coalbed methane reservoirs subjected to liquid nitrogen thermal shocking 被引量:3
3
作者 YAN Hong TIAN Li-peng +3 位作者 FENG Rui-min Hani MITRI CHEN Jun-zhi ZHANG Bo 《Journal of Central South University》 SCIE EI CAS CSCD 2020年第6期1846-1860,共15页
Thermal shocking effect occurs when the coalbed methane(CBM)reservoirs meet liquid nitrogen(LN2)of extremely low temperature.In this study,3D via X-ray microcomputer tomography(μCT)and scanning electron microscope(SE... Thermal shocking effect occurs when the coalbed methane(CBM)reservoirs meet liquid nitrogen(LN2)of extremely low temperature.In this study,3D via X-ray microcomputer tomography(μCT)and scanning electron microscope(SEM)are employed to visualize and quantify morphological evolution characteristics of fractures in coal after LN2 thermal shocking treatments.LN2 thermal shocking leads to a denser fracture network than its original state with coal porosity growth rate increasing up to 183.3%.The surface porosity of theμCT scanned layers inside the coal specimen is influenced by LN2 thermal shocking which rises from 18.76%to 215.11%,illustrating the deformation heterogeneity of coal after LN2 thermal shocking.The cracking effect of LN2 thermal shocking on the surface of low porosity is generally more effective than that of high surface porosity,indicating the applicability of LN2 thermal shocking on low-permeability CBM reservoir stimulation.The characteristics of SEM scanned coal matrix in the coal powder and the coal block after the LN2 thermal shocking presented a large amount of deep and shallow progressive scratch layers,fracture variation diversity(i.e.extension,propagation,connectivity,irregularity)on the surface of the coal block and these were the main reasons leading to the decrease of the uniaxial compressive strength of the coal specimen. 展开更多
关键词 liquid nitrogen thermal shocking coalbed methane micro fracture 3D via X-ray microcomputed tomography
下载PDF
Effect of Nonequilibrium Condensation of Moist Air on the Boundary Layer in a Supersonic Nozzle 被引量:7
4
作者 ShigeruMatsuo ShenYu 《Journal of Thermal Science》 SCIE EI CAS CSCD 1997年第4期260-272,共13页
When condensation occurs in supersonic flow fields, the flow is thected by the latent heat released. In the present study, Navier-Stokes equations were solved numerically using a 3rd-order MUSCL type TVD finitediffere... When condensation occurs in supersonic flow fields, the flow is thected by the latent heat released. In the present study, Navier-Stokes equations were solved numerically using a 3rd-order MUSCL type TVD finitedifference scheme with a second-order fractionabetep for time integration. Baldwin-Lomax model, that is the algebraic model, called the zero equation model was used in the computations. The effects of initial conditions (initial degree of supersaturation and total temperature in the reservoir) on condensing fiow of moist air in a supersonic circular half nozzle were investigated. In this case, the effect of condensation on the boundary layer was also discussed in detail. As a result, the simulated flow fields were compared with experimental data in good agreement, and the velocity and temperature profiles were largely changed by condensation. 展开更多
关键词 numerical simulation compressible flow CONDENSATION boundary layer moist air
原文传递
上一页 1 下一页 到第
使用帮助 返回顶部