红外与激光工程
紅外與激光工程
홍외여격광공정
INFRARED AND LASER ENGINEERING
2014年
9期
2883-2888
,共6页
激光辐照%飞行靶%热传导%温度场%有限容积法
激光輻照%飛行靶%熱傳導%溫度場%有限容積法
격광복조%비행파%열전도%온도장%유한용적법
laser irradiating%flying target%heat conduction%temperature field%finite volume method
以地基激光辐照飞行靶为研究背景,建立激光迎面辐照和横向辐照靶目标两种交汇场景,考虑激光辐照面域和功率密度分布随靶目标飞行的变化,求解激光辐照参数,建立热传导模型;利用有限容积法,得到飞行靶三维温度场的数值解,分析目标运动性对温度场分布的影响。不同于激光辐照静止目标,辐照参数变化对温度场分布有较大的影响:随着靶目标的飞行,辐照面积逐渐减小,平均功率密度逐渐增加,目标温升速率不断增加;光束与靶目标夹角的变化,引起光束强度空间分布的变化,从而影响温升区域的变化。
以地基激光輻照飛行靶為研究揹景,建立激光迎麵輻照和橫嚮輻照靶目標兩種交彙場景,攷慮激光輻照麵域和功率密度分佈隨靶目標飛行的變化,求解激光輻照參數,建立熱傳導模型;利用有限容積法,得到飛行靶三維溫度場的數值解,分析目標運動性對溫度場分佈的影響。不同于激光輻照靜止目標,輻照參數變化對溫度場分佈有較大的影響:隨著靶目標的飛行,輻照麵積逐漸減小,平均功率密度逐漸增加,目標溫升速率不斷增加;光束與靶目標夾角的變化,引起光束彊度空間分佈的變化,從而影響溫升區域的變化。
이지기격광복조비행파위연구배경,건립격광영면복조화횡향복조파목표량충교회장경,고필격광복조면역화공솔밀도분포수파목표비행적변화,구해격광복조삼수,건립열전도모형;이용유한용적법,득도비행파삼유온도장적수치해,분석목표운동성대온도장분포적영향。불동우격광복조정지목표,복조삼수변화대온도장분포유교대적영향:수착파목표적비행,복조면적축점감소,평균공솔밀도축점증가,목표온승속솔불단증가;광속여파목표협각적변화,인기광속강도공간분포적변화,종이영향온승구역적변화。
Taking ground-based laser irradiating flying target as the background, the encounter scenes were established which included head on irradiating scene and transverse irradiating scene. Considering the varying of irradiating area and power destiny distributing, the laser irradiating parameters were solved, and the heat conduction model was established. The numerical simulation of three-dimensional temperature field of flying target was calculated by the finite volume method. The influence of target moving on temperature field was analyzed. Different from laser irradiating stationary target, the varying of irradiating parameters has a great influence on temperature field distribution. As the target moving, the values of irradiating area decrease gradually, and the values of average power density and the rate of temperature rising increase gradually. The spacial profile of laser beam and temperature rising area are different because of the difference of angle between laser beam and target.