实验流体力学
實驗流體力學
실험류체역학
JOURNAL OF EXPERIMENTS IN FLUID MECHANICS
2014年
2期
90-94
,共5页
马兆侠%黄洁%石安华%苏铁%柳森
馬兆俠%黃潔%石安華%囌鐵%柳森
마조협%황길%석안화%소철%류삼
超高速撞击%温度%光谱%辐射特性%反溅碎片云
超高速撞擊%溫度%光譜%輻射特性%反濺碎片雲
초고속당격%온도%광보%복사특성%반천쇄편운
hypervelocity impact%temperature%spectrum%radiation characteristic%ricochet debris cloud
通过超高速撞击试验,获得了铝球撞击铝板反溅粒子云团在250~340nm波段的辐射特征光谱。在该波段辨认出铝原子的六条特征谱线,并对其伴线进行了解耦。根据所测光谱数据,使用多谱线法测量出不同撞击条件下的超高速撞击反溅粒子云团的温度,发现超高速撞击反溅粒子云团温度随弹丸直径和撞击速度的增加而增加;相较弹丸直径,反溅粒子云团温度对撞击速度更加敏感;最后拟合出反溅粒子云团温度与撞击参数之间的经验公式。对每条谱线波峰和整个波段分别进行了积分,研究发现谱线波峰积分强度、整个波段积分强度均与弹丸动能呈线性关系,并获得了谱线波峰积分强度与撞击动能之间的斜率系数,该系数可以表征在超高速撞击条件下该峰值的辐射效率。最后结合所得超高速撞击反溅粒子云团温度经验公式推导出基态原子数与撞击参数之间的关系,在此基础上探讨了超高速撞击反溅粒子云团原子离化率、气化率与撞击参数的关系。
通過超高速撞擊試驗,穫得瞭鋁毬撞擊鋁闆反濺粒子雲糰在250~340nm波段的輻射特徵光譜。在該波段辨認齣鋁原子的六條特徵譜線,併對其伴線進行瞭解耦。根據所測光譜數據,使用多譜線法測量齣不同撞擊條件下的超高速撞擊反濺粒子雲糰的溫度,髮現超高速撞擊反濺粒子雲糰溫度隨彈汍直徑和撞擊速度的增加而增加;相較彈汍直徑,反濺粒子雲糰溫度對撞擊速度更加敏感;最後擬閤齣反濺粒子雲糰溫度與撞擊參數之間的經驗公式。對每條譜線波峰和整箇波段分彆進行瞭積分,研究髮現譜線波峰積分彊度、整箇波段積分彊度均與彈汍動能呈線性關繫,併穫得瞭譜線波峰積分彊度與撞擊動能之間的斜率繫數,該繫數可以錶徵在超高速撞擊條件下該峰值的輻射效率。最後結閤所得超高速撞擊反濺粒子雲糰溫度經驗公式推導齣基態原子數與撞擊參數之間的關繫,在此基礎上探討瞭超高速撞擊反濺粒子雲糰原子離化率、氣化率與撞擊參數的關繫。
통과초고속당격시험,획득료려구당격려판반천입자운단재250~340nm파단적복사특정광보。재해파단변인출려원자적륙조특정보선,병대기반선진행료해우。근거소측광보수거,사용다보선법측량출불동당격조건하적초고속당격반천입자운단적온도,발현초고속당격반천입자운단온도수탄환직경화당격속도적증가이증가;상교탄환직경,반천입자운단온도대당격속도경가민감;최후의합출반천입자운단온도여당격삼수지간적경험공식。대매조보선파봉화정개파단분별진행료적분,연구발현보선파봉적분강도、정개파단적분강도균여탄환동능정선성관계,병획득료보선파봉적분강도여당격동능지간적사솔계수,해계수가이표정재초고속당격조건하해봉치적복사효솔。최후결합소득초고속당격반천입자운단온도경험공식추도출기태원자수여당격삼수지간적관계,재차기출상탐토료초고속당격반천입자운단원자리화솔、기화솔여당격삼수적관계。
The atomic emission spectrum of ricochet debris cloud,which was from aluminum plate subjected to hypervelocity impact by aluminum projectile,was obtained by transient spec-troscopy during hypervelocity impact test.The waveband range of spectrum which achieved in the test was 250~340nm.By analyzing the spectrum,six aluminum spectrum peaks were distin-guished from the emission spectrum and two coupling spectrum peaks were decoupled.With the aluminum spectrum constants and intensity of the six peaks,the ricochet debris cloud tempera-tures were diagnosed separately in different impact condition by using the multiple spectrum peaks method.It was found that the temperature would increase when the projectile diameter in-creased and it would increase with the impact velocity increasing,too.By analyzing the test re-sults of different projectile diameter,it was found that the ricochet debris cloud temperature was acutely sensitive to impact velocity.Based on the data achieved in the test,experiential formula describing relationships among ricochet debris cloud temperature,projectile diameter and impact velocity was obtained.Then the radiation characteristics of ricochet debris cloud were studied, every spectrum peak was integrated and the spectrum in the range of 250~340nm was integrat-ed,too.It was found that the spectrum peaks integral,the waveband integral of 250~340nm and impact kinetic energy behave in a linear fashion.The slopes of the spectrum peaks integral to impact kinetic energy were obtained and it could be considered as the radiation efficiency of every spectrum peak in hypervelocity impact.Finally,taking the experiential formula of ricochet debris cloud temperature into consideration,the relation between atom number in the ground state and impact parameter was deduced.The relations among ionization rate,gasification rate and impact parameters were explored.The conclusions would provide technical support for the further studies of the particular cloud temperature produced by hypervelocity impact and the impact parameters deducibility from impact radiation.