星际A型CH3CN—H2含超精细能级的碰撞跃迁速率系数的理论计算

本文作者利用ＩＯＳ近似模型，计算了星际分子云条件下Ａ型ＣＨ３ＣＮ－Ｈ２含超精细能级的碰撞跃迁速率系数，温度范围是２０Ｋ－１４０Ｋ，为研究分子云与恒星形成区的物理、化学性质提供了有用的基础分子数据。     

星际E型CH3CN与H2的碰撞跃迁速率系数的理论计算

继本文作者对星际Ａ型ＣＨ３ＣＮ与Ｈ２含超精细能级的碰撞过程的研究之后，又计算了星际分子云条件下Ｅ型ＣＨ３ＣＮ与Ｈ２的碰撞跃迁速率系数。为研究分子云与恒星形成区的物理、化学性质提供了有用的基础分子数据。     

星际分子正—NH3和He的超精细跃迁碰撞截面和速率系数的理论计算

本文采用Ｒ矩阵传播方法，通过求解ＣＳ近似下的耦合方程，计算了星际分子云条件下正－ＮＨ３分子和Ｈｅ碰撞的超精细跃迁碰撞截面和速率系数，为研究天体的信息提供需用的基础数据。     

CALCULATION OF VARIABLE DRAG AND HEAT-TRANSFER COEFFICIENTS IN METEORIC PHYSICS EQUATIONS

The conservation of the ablation parameter is one of the main assumptions of the classical physical theory of meteors (PTM). But this value does vary dramatically on meteoroids trajectories for the most part of them. The drag and heat-transfer coefficients in the basic equations of PTM are considered from the gasdynamical point of view and mathematically modeled in the present paper. Analytical approximations of the drag and heat transfer coefficients valid for any flow regimes and separate approximation of the drag coefficient for free-molecule regime are offered and discussed. They use the Reynolds number as the main parameter characterizing flow regimes. The variations of coefficients result in the variation of the ablation parameter by 100% for meteoroids, passing all the flow regimes. The importance of correct calculation of the coefficients for meteoroids motion modeling was demonstrated by the numerical examples.     

1997年日全食光谱观测仪器方案计算

本文介绍了为将已有的日食光谱仪主要部件用于1997年漠河日全食光谱观测而做的三种仪器设计方案,涉及定天镜位置、成象系统和光谱仪的光路安排。并与1983年日全食的情况对比,讨论其可行性及对观测和结果的影响。最后根据实际情况决定了观测采用的方案。