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Rotational Relaxation of N_2 Behind a Strong Shock Wave

机译:强冲击波后N_2的旋转弛豫

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摘要

Using an existing expression for the state-to-state rotational transition rate coefficients, which is derived from the experimental data taken at temperatures equal to or below 1500 K, the master equation for rotational states is integrated with time for N_2. The postshock temperature considered is from 400 to 128,000 K. From the numerical solutions of the master equation, the effective collision numbers and characteristic relaxation times are determined. The results show that the effective collision number varies from about 4 at 400 K to about 700 at 128,000 K. The product of the rotational relaxation time and pressure is determined to be 2.47 X 10~(-14)T~(1.692) atm • s. The calculated rotational relaxation time is larger than the vibrational relaxation time at temperatures above 12,000 K, but is believed to be only hypothetical there because vibration-rotation coupling will pull the temperatures of these two modes together. The present model approximately reproduces the rotational temperature values measured in a shock tube by Sharma and Gillespie and by Fujita et al. up to a postshock temperature of 90,000 K.
机译:使用从等于或低于1500 K的温度下获得的实验数据得出的状态到状态的旋转过渡速率系数的现有表达式,旋转状态的主方程与N_2的时间积分。考虑的震后温度为400至128,000K。根据主方程的数值解,可以确定有效碰撞数和特征驰豫时间。结果表明,有效碰撞数在400 K时约4到128,000 K时约700。旋转弛豫时间和压力的乘积确定为2.47 X 10〜(-14)T〜(1.692)atm• s。所计算出的旋转弛豫时间大于温度高于12,000 K时的振动弛豫时间,但据认为只是假想的,因为振动-旋转耦合会将这两种模式的温度拉在一起。本模型近似再现了Sharma和Gillespie以及Fujita等人在减震管中测得的旋转温度值。高达90,000 K的余震温度。

著录项

  • 来源
    《Journal of Thermophysics and Heat Transfer》 |2004年第4期|p.527-533|共7页
  • 作者

    Chul Park;

  • 作者单位

    Department of Aerospace Engineering, Korea Advanced Institute of Science and Technology, Daejeon 305-701, Korea;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);美国《生物学医学文摘》(MEDLINE);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 理论物理学;
  • 关键词

  • 入库时间 2022-08-18 03:01:38

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