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Composite material ; barrel ; interior ballistics ; numerical heat transfer ; erosion and service life

复合材料;身管;内弹道学;数值传热;烧蚀与寿命

On the basis of the lumped physical-mathematical model of interior ballistics given in reference 1,this paper gives a detailed discussion about the conditions leading to the formation of pressure plateau in the combustion chamber of a RLPG,and derives the analytical relationship between the jet area and other parameters under which the pressure plateau can be formed.

在文献1建立的RLPG集总参数内弹道学数学物理模型的基础上,对RLPG压力平台产生的条件进行了详细的探讨,推导了满足压力平台的喷孔面积与膛内其它参量之间的解析关系式,编制了计算程序,处理了计算过程中所产生的压力振荡问题,获得了工程设计中实用的产生压力平台的中心杆半径与其行程的变化关系曲线。

Flat plate steady mathematical model and non steady symmetric model are presented, the analytical solution of temperature of powder is derived on the basis of non steady symmetric model in spheroidal coordinates with the methods of mathematical transformation and principle of superposition .

对点火问题进行研究,给出了两种点火的数学模型;平板定常模型和球对称非定常模型。从火药颗粒的球对称非定常模型出发,利用叠加原理和数学变换导出了火药颗粒表面温度的分析解。该研究对深入研究点火理论和起始弹道学有一定的作

Based on water-entry dynamic and water-entry ballistic theories,the oblique water-entry process of disk ogive is simplified and a wetted correction factor is introduced in order to accord with the true water pile phenomena,and an oblique water-entry impact model coupled with ballistic and dynamic models are established.

以冲击体入水动力学和入水弹道学理论为基础,针对平头尖拱体入水冲击这个复杂物理现象,引入体现液面隆起现象的沾湿因子,用等效液面代替自由水平液面,建立了斜入水高速冲击的运动学和动力学冲击模型,其中动力学模型是根据平头尖拱体沾湿面的具体几何形状而建立。

Based on water-entry dynamic and water-entry ballistic theories, the oblique water-entry process of disk ogive is simplified and a wetted correction factor is introduced in order to accord with the true water pile phenomena, and an oblique water-entry impact model coupled with ballistic and dynamic models are established. According to the exact geometric shape of the wetted body surface, the dynamic model is established.

以冲击体入水动力学和入水弹道学理论为基础,针对平头尖拱体入水冲击这个复杂物理现象,引入体现液面隆起现象的沾湿因子,用等效液面代替自由水平液面,建立了斜入水高速冲击的运动学和动力学冲击模型,其中动力学模型是根据平头尖拱体沾湿面的具体几何形状而建立。

The trajectory, or path, of a projectile is subject to the forces of gravity, drag, and lift.

弹道学是研究射弹的飞行,弹道是射弹在重力、拖曳力和升力作用下的飞行路线。

The projectile motion touching the bore wall with the bourrelet, an important project in ballistics, is included in the analysis solution to a general Ricatti equation.

将在弹道学中具有重要地位的弹丸前定心部紧贴膛壁的运动问题〓,首次归结为一般的Ricatti方程的求解问题,找到了相应的足够精确的解析解。

This article is mainly on developing a new pyrotechnic exhaust composition, after analyzing some base-bleeding agent existing.

本文首先从外弹道学角度对烟火底排减阻机理进行了深入研究,从理论上探讨了降低底阻的技术途径。

In the flying course of the low-speed revolving rocket, deflective flow willappear due to the nutation effect, the method of calculating the deflective flow based on the exterior ballistics is given, and the simulation result with some examples is also stated.

低速旋转火箭弹在飞行过程中,由于章动因素的影响产生偏流。本文根据外弹道学理论给出偏流的计算方法,并结合实例给出仿真模拟结果,通过计算分析偏流对多管火箭弹飞行轨迹的影响

This thesis proposes a kind of soft firing technology , which combines interior ballistics with atmospheric pressure transmission theory , utilizing the energy of advancing primer ignition of piston promoting pill to counteract the counterforce of firing pill , utilizing unilateral valve on the piston to adjust automatically the gas pressures of two connected chamber in series in front and at the back of the piston, thus achieving the goal of reducing composition of forces of gun bore and increasing initial velocity of pill.

本论文提出一种软发射技术,是将气压传动理论和经典内弹道学相结合,利用活塞推动弹丸前冲击发的能量来抵消发射弹丸所产生的反作用力,利用活塞上的单向阀自动调节活塞前后两个串联药室的气体压力,从而达到减小炮膛合力和提高弹丸初速的目的。

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