航天飞机主发动机羽流原子谱线展宽碰撞截面的计算

T.C. Dean, C. Ventrice
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引用次数: 0

摘要

利用Kunc提出的有效重心力相互作用势,研究了分子摄动器加宽碰撞线截面的解析方法。伦纳德-琼斯势一直被用来描述原子间的相互作用。对SSME羽流环境的主要成分之一H/ sub2 /的几种原子进行了截面测定,并与实验数据进行了比较。在实验误差范围内与大多数原子种类的实验数据一致。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Calculation of collision cross sections for atomic line broadening in the plume of the Space Shuttle main engine (SSME)
An analytical method for determining the cross sections for collision line broadening by molecular perturbers is investigated using effective central force interaction potentials as proposed by Kunc. The Lennard-Jones potential is used throughout to describe the interatomic interactions. These cross sections are determined for several atomic species with H/sub 2/, one of the principal constituents of the SSME plume environment, and compared with experimental data. Agreement with experimental data within the range of experimental error is obtained for most atomic species.
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