利用FLUENT软件,使用湍流模型和VOF(volume of fluid)模型对水下点火固体火箭发动机的气液两相流场进行数值分析,对点火初期喷管中燃气的流动过程和燃气泡的发展过程进行了仿真,数值模拟了固体火箭发动机尾流场燃气密度、压力和温度的...利用FLUENT软件,使用湍流模型和VOF(volume of fluid)模型对水下点火固体火箭发动机的气液两相流场进行数值分析,对点火初期喷管中燃气的流动过程和燃气泡的发展过程进行了仿真,数值模拟了固体火箭发动机尾流场燃气密度、压力和温度的分布规律。研究表明:点火初期,喷管内流场将有一个完整激波建立的过程,除此之后的喷管尾流区域,由于气体受到压力扰动的影响,激波结构被破坏,没有形成连续的膨胀—压缩波;射流过程中燃气泡头部一直保持较大直径,中部燃气通道存在随轴向周期性的膨胀-压缩现象;喷管尾流区,各流动参数出现不同程度的振荡现象:喷管出口燃气密度受外界水的压缩及传质传热的影响,出现峰值后逐渐稳定;喷管出口燃气总压由于受水环境的急剧压缩,在喷管出口附近形成一个高压区;喷管出口燃气温度经三次周期变化后,温度逐渐降至1 750K以内。展开更多
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 &...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.展开更多
文摘利用FLUENT软件,使用湍流模型和VOF(volume of fluid)模型对水下点火固体火箭发动机的气液两相流场进行数值分析,对点火初期喷管中燃气的流动过程和燃气泡的发展过程进行了仿真,数值模拟了固体火箭发动机尾流场燃气密度、压力和温度的分布规律。研究表明:点火初期,喷管内流场将有一个完整激波建立的过程,除此之后的喷管尾流区域,由于气体受到压力扰动的影响,激波结构被破坏,没有形成连续的膨胀—压缩波;射流过程中燃气泡头部一直保持较大直径,中部燃气通道存在随轴向周期性的膨胀-压缩现象;喷管尾流区,各流动参数出现不同程度的振荡现象:喷管出口燃气密度受外界水的压缩及传质传热的影响,出现峰值后逐渐稳定;喷管出口燃气总压由于受水环境的急剧压缩,在喷管出口附近形成一个高压区;喷管出口燃气温度经三次周期变化后,温度逐渐降至1 750K以内。
基金supported by the National Natural Science Foundation of China (No.11574159)the Open Fund of the State Key Laboratory of High Field Laser Physics,China (Shanghai Institute of Optics and Fine Mechanics)the Special Research Foundation of the Central University of Nankai University (No.63191108)。
文摘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.
