共查询到15条相似文献,搜索用时 62 毫秒
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为了优化二级轻气炮的设计参数和工作参数,必须进行数值模拟。本文介绍了准一维不定常流的Lagrangian算法,讨论了数值模拟中的若干问题,分析了气动过程。根据我们的数值模拟,归纳了影响气炮性能的一些基本规律,可供选择工作参数时综合分析。 相似文献
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气相爆轰驱动二级轻气炮内弹道数值模拟 总被引:1,自引:1,他引:1
二级轻气炮是超高速弹丸驱动技术中使用最广泛的技术之一, 它在超高速气动物理现象及材料高速碰撞下力学性能的实验研究和验证方面起着不可或缺的作用. 中国科学院力学研究所基于爆轰驱动方法研制了一座大型二级轻气炮, 可弥补高压气体驱动能力有限和火药使用受限的不足. 本文基于经过实验验证的准一维数值模拟方法, 详细研究了该设备的内弹道动力学参数及发射性能, 并探讨了不同发射方法及装填参数对设备性能的影响规律和机理. 研究结果表明, 氢氧爆轰驱动相比于高压气体驱动具有明显优势; 不同爆轰驱动方式对弹丸发射性能影响较小, 但其影响到整个设备的强度设计; 对装填运行参数的研究表明增大爆轰段充气压力可以有效加强轻气炮发射性能, 而活塞质量变化对发射速度的影响较为复杂, 轻气炮实际运行中受设备设计指标及模型材料性能的限制, 优化过程中需要同时调整3种参数以达到轻气炮最佳性能. 相似文献
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Flow, Turbulence and Combustion - In this communication the authors have given a theory of internal ballistics of a high velocity light gas gun in which the column of conventional propellant gas... 相似文献
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二级轻气炮是一种常见的超高速发射装置,多年来其数值研究大多采用简化一维模型,鲜有三维有限元模型。以14 mm口径高压气体驱动二级轻气炮为研究对象,采用耦合欧拉-拉格朗日(coupled Eulerian-Lagrangian, CEL)算法,根据膜片破裂与否,将二级轻气炮模型解耦为2个分级三维数值模型。为确定实验难以测得的参数(材料摩擦因数和膜片破膜压力),设计正交试验,拟合确定活塞与泵管间摩擦因数为0.82,弹丸与发射管摩擦因数为0.30和膜片破膜压力为11.73 MPa。正交结果表明,摩擦因数对计算结果影响较大,在高压气体驱动二级轻气炮的计算中不应忽略。通过上述方法建立数字化高压气体驱动二级轻气炮,完整复现气炮发射过程,计算的弹丸终速与实验结果吻合度高。选取验证工况详细分析了气炮发射过程内流场变化,并呈现关键时刻的压力云图。该气炮简化方法、分级思想和关键参数确认方法可推广应用于固体发射药驱动、爆轰驱动等其他驱动形式的二级/多级轻气炮。
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B. V. Novozhilov 《Journal of Applied Mechanics and Technical Physics》1970,11(4):585-590
An integral equation is obtained for the nonsteady-state combustion velocity of a powder. It is shown that the effect of a variable tangential stream of gases on the rate of burning (nonsteady-state erosion) can be calculated in a similar way as for the change of pressure. The solution of the equation in linear approximation is considered (rate of burning differs slightly from steady-state).Translated from Zhurnal Prikladnoi Mekhaniki i Teknicheskoi Fiziki, No. 4, pp. 73–78, July–August, 1970. 相似文献
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A method for finding exact solutions of the equations of gas dynamics with a linear velocity field is proposed. This method was used to find exact solutions for one submodel of the evolutionary type which was fully integrated for the case of a polytropic gas. Examples of particle motion for the obtain exact solutions are given. 相似文献
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This paper contains an exposition of the results of numerical modeling of the nonstationary two-stage flow of an underexpanded jet into the surrounding space by the method of coarse particles. A comparison is made with the results of experiment.Translated from Izvestiya Akademii Nauk SSSR, Mekhanika Zhidkosti i Gaza, No. 4, pp. 153–156, July–August, 1978. 相似文献
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We consider the system of moments associated with the relativistic Boltzmann-Chernikov equation. Using the particular symmetric
form obtained by the closure procedure of Extended Thermodynamics we deduce a lower bound for the maximum velocity of wave
propagation in terms of the number of moments for a non-degenerate gas. When the number of moments increases this velocity
tends to the speed of light. We also give the lower bound estimate in the limit cases of ultrarelativistic fluids and in the
non relativistic approximation.
Received September 28, 1998 相似文献
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The linear relation between the particle concentration and the output voltage of a light extinctiometer used to measure particle concentrations has been derived and calibrated. A time integration method was introduced to determine the characteristic parameter of such a measuring system. This characteristic parameter which is proportional to the extinction coefficient is found to be in good agreement with its theoretical value. As an example, in a vertical tube the increasing particle concentration was measured behind a developing flat interface between a gas and a gas-particle mixture as a function of time.On leave from East China Institute of Technology, Nanjing 210014, The People's Republic of China 相似文献