导弹弹射气体冲击载荷实验与仿真研究

设计一套模拟发射筒内建压过程的装置,使之能够模拟不同建压速度、不同终值压强时的发射筒内建压过程,进而对导弹弹射过程中导弹尾罩和其他结构受到的气体冲击载荷进行地面冷实验。分别对四种不同初始条件下的建压过程进行了实验,并对一种情况进行了数值模拟仿真。结果显示,实验设备通过调节柱塞两侧初始压力差和高压气缸初始压力,可以实现对不同建压速率、不同终值压强的模拟;在建压过程中模拟发射筒内存在明显涡流,尾罩中间部位受压更大,变形时间相较于升压时间存在明显滞后。     

丁羟推进剂花板浇注过程数值仿真

为研究丁羟推进剂浇注过程中流场结构,使用改进后的Herschel-Bulkley黏度模型对药浆花板浇注过程进行了数值模拟,并与实验数据进行了对比。结果显示:在通过花板孔后药浆会发生汇流,汇流后的药浆在重力作用下在发动机壳体内堆积,堆积表面呈现不规则的凹凸状,但在重力作用下,药浆会逐渐流平并填满空腔,未形成空洞。被花板分割的药条一部分汇聚后沿翼片间凹槽向下流动,一部分直接向下流动,流动过程中出现拉伸断裂的现象。浇注所需总时间为104 min,浇注药浆总质量为160.3 kg,平均质量流率为5.4 g·(hole·min)-1,仿真计算值与实测值误差分别为8.65%、2.06%和5.93%。     

Femtosecond laser processing stainless steel foil and its Fourier spectrum detection

In this paper, we use femtosecond laser pulse to scribe 304 stainless steel foil, detect the Fourier transform infrared spectrum of the sample before and after processing, confirm the "cold processing" and "thermal processing" and their mutual conversion, and determine the "cold processing" parameter window. The ablation threshold and incubation coefficient of 304 stainless steel foil are calculated, and the effects of scanning speed and effective pulse number on the ablation threshold are analyzed. The ANSYS software is used to simulate the radial and axial temperature distributions of the surface on 304 stainless steel foil sample and the heat-affected zone with a femtosecond laser fluence of 10 J/cm2 and an effective number of pulses of 1 200 are obtained. In the aspect of spectral detection, the Fourier transform infrared spectra of the sample before and after processing are measured and two processing mechanisms of "cold processing" and "hot processing" are confirmed, which proves that we can achieve the conversion between "cold processing" and "hot processing" by changing the laser fluence and determine the "cold processing" laser fluence range.     

燃气凝相颗粒对固体火箭发动机尾流场影响的数值分析

利用FLUENT软件对燃烧产物中含Al_2O_3凝相粒子的固体火箭发动机尾流场结构进行数值计算,与纯气相作用下的尾流场结构进行比较分析,分析Al_2O_3粒子对固体火箭发动机尾流场结构的影响。结果表明:随着Al_2O_3凝相粒子的加入,尾流场膨胀压缩波系的个数减少,波系的膨胀半径增大,波系的长度增加,尾流核心区的长度增大。尾流场的马赫数减小,温度升高。