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Compared with the conventionally gaseous or liquid working media, the specific internal energy of supercritical carbon dioxide (SCD) is higher at the same temperature and pressure, and the critical temperature of carbon dioxide is close to room temperature, making SCD a potential new working medium for pneumatic launch. To analyze the feasibility of this conception, an analytical model of a pneumatic catapult is established on basis of the conservations of mass and energy. The model consists of a high-pressure chamber and a low-pressure chamber connected by multiple valves, and there is a movable piston in the low-pressure chamber that can push an aircraft to accelerate. The effects of the launch readiness state of SCD in the high-pressure chamber, the initial volume of the low-pressure chamber and the valve control on the movement of the aircraft are analyzed. It is found that there is a restrictive relation between the temperature and pressure of the launch readiness state of SCD, i.e., there is a maximum allowable launch readiness pressure when the launch readiness temperature is fixed. If this restrictive relation is not satisfied, the working medium in the low-pressure chamber will drop to its triple point within a few milliseconds, leading to a launch failure. Owing to this restrictive relation, there is an optimal launch readiness state of SCD with the highest working capacity for any allowable launch readiness temperature. The pressure of the low-pressure chamber will decrease significantly as the initial volume increases, leading to a decreased acceleration of the aircraft. The ac-celeration can be controlled below a critical value by a designed sequential blasting technique of multiple valves. The calculated results show that a 500 kg aircraft can be accelerated from 0 to 58 m/s in 0.9 s with 36 kg of carbon dioxide. This research provides a new technique for the controllable cold launch of an aircraft. 相似文献
303.
《防务技术》2020,16(2):381-391
This study investigates the effect of tool rotational speed (TRS) on particle distribution in nugget zone (NZ) through quantitative approach and its consequences on the mechanical property of friction stir welded joints of AA6092/17.5 SiCp-T6 composite. 6 mm thick plates are welded at a constant tool tilt angle of 2° and tool traverse speed of 1 mm/s by varying the TRS at 1000 rpm, 1500 rpm and 2000 rpm with a taper pin profiled tool. Microstructure analysis shows large quantity of uniformly shaped smaller size SiC particle with lower average particle area which are homogeneously distributed in the NZ. The fragmentation of bigger size particles has been observed because of abrading action of the hard tool and resulting shearing effect and severe stress generation due to the rotation of tool. The particles occupy maximum area in the matrix compared to that of the base material (BM) due to the redistribution of broken particles as an effect of TRS. The migration of particles towards the TMAZ-NZ transition zone has been also encountered at higher TRS (2000 rpm). The microhardness analysis depicts variation in average hardness from top to bottom of the NZ, minimum for 1500 rpm and maximum for 2000 rpm. The impact strength at 1000 rpm and 1500 rpm remains close to that of BM (21.6 J) while 2000 rpm shows the accountable reduction. The maximum joint efficiency has been achieved at 1500 rpm (84%) and minimum at 1000 rpm (68%) under tensile loading. Fractographic analysis shows mixed mode of failure for BM, 1000 rpm and 1500 rpm, whereas 2000 rpm shows the brittle mode of failure. 相似文献
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单站纯方位目标跟踪系统可观测性分析 总被引:1,自引:0,他引:1
针对单站纯方位目标跟踪系统的可观测性,在研究国内外有关状况的基础上,给出了单站纯方位目标运动分析的问题描述,综述了国内外的研究和发展情况,给出了由观测可观测性的一些结论和证明.其中对某些经典的结论给出了简单、明了的证明方法,这些有助于该问题的深入理解和研究. 相似文献
307.
改进了线性方程组迭代解法的矩阵形式.以最简单的Jacobi迭代法的迭代矩阵为基础,只需经过简单的加减和数乘运算就可得到Seidel和SOR的迭代过程,使得算法新形式的求解过程数学意义非常明确,表达形式也非常简洁,这样不仅便于理解记忆,还非常有利于编程实现。改进后的矩阵迭代形式求解计算量为:Seidel需要大约n2次乘除法.SOR约为2n2次乘除法,且改进后的Seidel迭代法和SOR方法存储空间也较传统形式为少。 相似文献
308.
利用特征矩阵法对一维金属-介质光子晶体的特性进行了计算,发现此种光子晶体具有可见光透明,微波、紫外高反的光谱特性,而且存在比一维介质光子晶体更宽、反射更强的全向带隙. 相似文献
309.
以聚碳硅烷(PCS)/二乙烯基苯(DVB)为先驱体,采用快速升温裂解制备了3D-B Cf/SiC复合材料.结果证明:裂解升温速率的提高可以大大缩短制备周期,同时可以提高材料密度和形成较好的界面结合,从而提高材料的力学性能.制备得到的Cf/SiC材料室温弯曲强度达到556.7MPa. 相似文献
310.
文中研究了用离子减薄法制备NICALON(SiC)/A1预制丝的透射电镜(TEM)样品。结果表明:用离子减薄法制备含有性质非常不同的组元(如碳化硅-铝复合材料)TEM样品是一种方便、有效的方法。运用TEM初步分析了所制出的预制丝样品。 相似文献