共查询到17条相似文献,搜索用时 203 毫秒
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气相爆轰高阶中心差分-WENO组合格式自适应网格方法 总被引:1,自引:0,他引:1
研究一种高阶中心差分-WENO组合格式,并采用自适应网格方法进行二维和三维气相爆轰波的数值模拟.采用ZND爆轰模型的控制方程为包含化学反应源项的Euler方程组.组合格式在大梯度区采用WENO格式捕捉间断,在光滑区采用高阶中心差分格式提高计算效率.采用一种基于流场结构特征的自适应网格.计算结果,表明这种方法同时具有高精度、高分辨率和高效率的特点. 相似文献
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假设爆轰波阵面的法向速度是曲率的线性函数,在非结构四边形网格上采用水平集方法模拟爆轰波阵面的运动过程.水平集方程的曲率无关项采用正格式离散,曲率项采用伽辽金等参有限元方法空间离散,时间离散采用半隐格式.在笛卡儿网格和随机网格上,含曲率的水平集方程的离散格式为强一阶精度,重新初始化方程的离散格式精度为近似一阶精度.曲率收缩的不光滑界面和多个爆轰波阵面相互作用的算例说明格式可有效地模拟爆轰波与曲率相关的运动. 相似文献
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龙格库塔间断有限元方法在计算爆轰问题中的应用 总被引:1,自引:1,他引:0
构造求解带源项守恒律方程组的龙格库塔间断有限元(RKDG)方法,并分别结合源项的Strang分裂法和无分裂法数值求解模型守恒律方程和反应欧拉方程.为了和有限体积型WENO方法进行比较,设计计算源项的WENO重构格式.对一维带源项守恒律的计算表明,对于非刚性问题,RKDG方法比有限体积型WENO方法的误差更小;对于刚性问题,RKDG方法对于间断面位置的捕捉更为精确.对于一二维爆轰波问题的计算结果表明,RKDG方法对爆轰波结构的分辨和爆轰波位置的捕捉能力更强. 相似文献
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CTVD格式数值计算非均质炸药爆轰问题 总被引:3,自引:0,他引:3
将高分辨率激波捕捉格式CTVD格式拓展应用到非均质炸药爆轰的数值模拟问题.增加了化学反应率控制方程,引入Lee-Tarver点火成长模型,未反应的固体炸药和化学反应气体产物都使用JWL形式状态方程.数值模拟了非均质固体炸药PBX-9404和TATB的冲击起爆问题.获得了较高的爆轰波分辨率和光滑解区的数值精度,对具有复杂物态方程形式的固体炸药爆轰问题,CTVD格式具有简单实用、高效和高分辨的特点. 相似文献
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提出一种数值模拟凝聚炸药爆轰问题的单元中心型Lagrange方法.利用有限体积离散爆轰反应流动方程组,基于双曲型偏微分方程组的特征理论获得离散网格节点的速度与压力,获得的网格节点速度与压力用于更新网格节点位置以及计算网格单元边的数值通量.以这种方式获得的网格节点解是一种"真正多维"的理论解,是一维Godunov格式在二维Riemann问题的推广.有限体积离散得到的爆轰反应流动的半离散系统使用一种显-隐Runge-Kutta格式来离散求解:显式格式处理对流项,隐式格式处理化学反应刚性源项.算例表明,提出的单元中心型Lagrange方法能够较好地模拟凝聚炸药的爆轰反应流动. 相似文献
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提出一种在自由重映移动网格下的广义黎曼问题方法模拟反应流.该方法基于显式的自由重映移动网格广义黎曼问题的解.为保证在时间和空间上的高精度,应用广义黎曼问题方法构造数值通量.为保证反应区的高分辨率,采用变分法生成自适应移动网格.该方法不仅能够保证网格质量,而且能有效地避免任意拉格朗日—欧拉方法中由于显式重映过程而带来的数值误差.包括CJ爆轰及不稳定爆轰的数值实验说明该格式的精确性和鲁棒性,证明这种移动网格下的二阶广义黎曼问题方法可以较好地捕捉反应流的间断与光滑结构. 相似文献
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An improved two-dimensional space-time conservation element and solution element (CE/SE) method with second-order accuracy is proposed, examined and extended to simulate the detonation propagations using detailed chemical reaction models. The numerical results of planar and cellular detonation are compared with corresponding results by the Chapman-Jouguet theory and experiments, and prove that the method is a new reliable way for numerical simulations of detonation propagation. 相似文献
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为了研究高Mach数超燃冲压发动机和斜爆轰发动机的内流场燃烧流动机理,首先用CJ爆轰理论对超燃冲压发动机的内流场特性进行了理论分析,给出了燃烧室流场的气动规律,理论分析结果与现有实验结果吻合得非常好.其次,根据理论分析结果,提出了高Mach数超燃冲压发动机和斜爆轰发动机的气动设计原则.最后,根据提出的气动设计原则,设计了高Mach数斜爆轰发动机,飞行Mach数为9,对斜激波诱导燃烧机理开展了二维数值模拟研究.数值模拟结果表明,在高Mach数下,斜爆轰发动机燃烧室内可以得到稳定的燃烧流场. 相似文献
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An unstructured adaptive mesh flow solver, a finite element structure solver and a moving mesh algorithm were implemented in the numerical simulation of the interaction between a shock wave and a structure. In the past, this interaction is mostly considered as one-way in the sense that the shock causes a transient load on the structure while it is reflected uneffected by the impact. A fully coupled approach was implemented in the present work which can account for the effects associated with a mutual interaction. This approach included a compressible flow Eulerian solver of second order accuracy in finite volume formulation for the fluid and a Langargian solver in finite element formulation for the solid structure. A novel implementation of advancing front moving mesh algorithm was made possible with the introduction of a flexible and efficient quad-edge data structure. Adaptive mesh refinement was introduced into the flow solver for improved accuracy as well. Numerical results are further validated by theoretical analysis, experimental data and results from other numerical simulations. Grid dependency study was performed and results showed that the physical phenomena and quantities were independent of the numerical grid chosen in the simulations. The results illuminated complicated flow phenomena and structure vibration patterns, which in order to be detected experimentally require capabilities beyond those of the current experimental techniques. The numerical simulations also successfully modelled the aero-acoustic damping effects on the structure, which do not exist in previous numerical models. Further analysis of the results showed that the mutual interaction is not linear and that the non-linearity arises because the wave propagation in the fluid is not linear and it cascades a non-linear and non-uniform loading on the plate. Non-linearity intensifies when the plate is vibrating at high frequency while the wave propagation speed is low. 相似文献
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依据C-J(Chapman-Jouguet)理论,对爆轰问题中的气态爆轰产物和未反应炸药分别考虑不同的参考状态,并根据参考状态选用特定的Mie-Grüneisen状态方程。忽略化学反应过程,爆轰产物厚度为零的前导激波面以界面的形式存在。数值模拟中,爆轰波的演化分为波面传播以及与未反应介质相互作用两个部分。传播过程中,爆轰波的传播速度即恒定的爆速,爆轰产物在传播过程中瞬间形成,而相互作用过程则是通过Mie-Grüneisen多介质混合模型来计算爆轰波的持续冲击作用。借助于Mie-Grüneisen状态方程以及Mie-Grüneisen多介质混合模型,可以很好地模拟爆轰波的运动过程。对比理论参数及文献的计算结果发现,模拟结果具备较好的准确度。 相似文献
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The modified CCW relation is applied to analyzing the shock, detonation wave converging and the role of chemical reactions
in the process. Results indicate that the shock wave is strengthened faster than the detonation wave in the converging at
the same initial Mach number. Euler equations implemented with a detailed chemical reaction model are solved to simulate toroidal
shock and detonation wave converging. Gasdynamic characteristics of the converging are investigated, including wave interaction
patterns, observable discrepancies and physical phenomena behind them. By comparing wave diffractions, converging processes
and pressure evolutions in the focusing area, the different effects of chemical reactions on diffracting and converging processes
are discussed and the analytic conclusion is demonstrated through the observation of numerical simulations. 相似文献