光谱学与光谱分析
光譜學與光譜分析
광보학여광보분석
SPECTROSCOPY AND SPECTRAL ANALYSIS
2010年
4期
865-868
,共4页
彭志敏%杨乾锁%刘春%竺乃宜%姜宗林
彭誌敏%楊乾鎖%劉春%竺迺宜%薑宗林
팽지민%양건쇄%류춘%축내의%강종림
激波管%高温气体%光学多通道分析仪%分子光谱%AlO自由基
激波管%高溫氣體%光學多通道分析儀%分子光譜%AlO自由基
격파관%고온기체%광학다통도분석의%분자광보%AlO자유기
Shock tube%Heated air%Optical multi-channel analyzer%Molecular spectrum%AlO radical
爆轰驱动过程中产生的高温高压气流对铝质膜片、激波管壁产生烧蚀和冲刷作用,以致激波管壁、端盖上附有氧化铝等杂质,而高温下AlO自由基在气体分子的高速碰撞下被激发并产生强烈的辐射,从而干扰了高温气体辐射光谱的分析.用爆轰驱动加热技术将空气加热到4 000~7 000 K,利用多通道光学分析仪对AlO自由基辐射光谱进行分析,实验发现在460~530 nm波长范围内有多支辐射非常强烈的AlO自由基B~2∑~+-X~2∑~+(T_(00)=20 689 cm~(-1))带系辐射谱带,且每支谱带都由多个带头组成,带头间隔约为2 mn,带头处于高频位置并向低频方向伸延.通过实验与理论计算相结合,重点分析了AlO自由基B~2∑~+-X~2∑~+带系辐射光谱的结构特征.AlO自由基C~2∏_r-X~2∑~+(T_(00)=33 047 cm~(-1))带系辐射光谱处于270~335 nm波长范围内,其辐射强度相对于B~2∑~+-X~2∑~+带系较弱,并且与OH基A~2∑~+-X~2∏(T_(00)=32 682 cm~(-1))带系辐射光谱互相干扰而难以分辨,对该波段高温空气的辐射光谱分析产生不利的影响.
爆轟驅動過程中產生的高溫高壓氣流對鋁質膜片、激波管壁產生燒蝕和遲刷作用,以緻激波管壁、耑蓋上附有氧化鋁等雜質,而高溫下AlO自由基在氣體分子的高速踫撞下被激髮併產生彊烈的輻射,從而榦擾瞭高溫氣體輻射光譜的分析.用爆轟驅動加熱技術將空氣加熱到4 000~7 000 K,利用多通道光學分析儀對AlO自由基輻射光譜進行分析,實驗髮現在460~530 nm波長範圍內有多支輻射非常彊烈的AlO自由基B~2∑~+-X~2∑~+(T_(00)=20 689 cm~(-1))帶繫輻射譜帶,且每支譜帶都由多箇帶頭組成,帶頭間隔約為2 mn,帶頭處于高頻位置併嚮低頻方嚮伸延.通過實驗與理論計算相結閤,重點分析瞭AlO自由基B~2∑~+-X~2∑~+帶繫輻射光譜的結構特徵.AlO自由基C~2∏_r-X~2∑~+(T_(00)=33 047 cm~(-1))帶繫輻射光譜處于270~335 nm波長範圍內,其輻射彊度相對于B~2∑~+-X~2∑~+帶繫較弱,併且與OH基A~2∑~+-X~2∏(T_(00)=32 682 cm~(-1))帶繫輻射光譜互相榦擾而難以分辨,對該波段高溫空氣的輻射光譜分析產生不利的影響.
폭굉구동과정중산생적고온고압기류대려질막편、격파관벽산생소식화충쇄작용,이치격파관벽、단개상부유양화려등잡질,이고온하AlO자유기재기체분자적고속팽당하피격발병산생강렬적복사,종이간우료고온기체복사광보적분석.용폭굉구동가열기술장공기가열도4 000~7 000 K,이용다통도광학분석의대AlO자유기복사광보진행분석,실험발현재460~530 nm파장범위내유다지복사비상강렬적AlO자유기B~2∑~+-X~2∑~+(T_(00)=20 689 cm~(-1))대계복사보대,차매지보대도유다개대두조성,대두간격약위2 mn,대두처우고빈위치병향저빈방향신연.통과실험여이론계산상결합,중점분석료AlO자유기B~2∑~+-X~2∑~+대계복사광보적결구특정.AlO자유기C~2∏_r-X~2∑~+(T_(00)=33 047 cm~(-1))대계복사광보처우270~335 nm파장범위내,기복사강도상대우B~2∑~+-X~2∑~+대계교약,병차여OH기A~2∑~+-X~2∏(T_(00)=32 682 cm~(-1))대계복사광보호상간우이난이분변,대해파단고온공기적복사광보분석산생불리적영향.
There are some impurities such as aluminum dioxide adhering on the shock tube wall due to the ablating and heating of the aluminum diaphragm by high temperature gas. Under high temperature, the collision of AlO radicals with the gaseous mole-cules leads to transition of the electronic states and production of strong radiation, which disturb the analysis of radiation spec-trum of heated gases in shock tube. In the authors' experiments, the air in the test section with adhering aluminum dioxide was heated to some 4 000-7 000 K, the spectrum of AIO radical was obvious in the range of 460-530 nm, which corresponds to B ~2∑~+-X~2∑~+(T_(00) =20 689 cm~(-1) band. There were several band heads for this band, the interval of neighbor heads was some 2 nm, and all the band heads were with the shortest wavelength. The characteristics of B~2∑~+-X~2∑~+ band were explored in exper-iment and by theory. In addition, the spectrum of C~2∏_r-X~2∑~+(T_(00) =33 047 cm~(-1)) band was also investigated. The corre-sponding strength was lower than that of B~2∑~+-X~2∑~+ band, and the wavelength range of this band was some 270-335 nm where the radiation of A 2∑~+ -X~2∏ (T_(00)=32 682 cm~(-1)) band of OH radical also existed. This occurrence of the two bands in the same wavelength range is disadvantageous for the spectrum analysis.