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人-椅系统的动压计算问题
引用本文:张云然,吴桂荣.人-椅系统的动压计算问题[J].航空学报,1995,16(1):70-73.
作者姓名:张云然  吴桂荣
作者单位:航天医学工程研究所, 北京, 100094
摘    要:通过大量的分析、计算,提出了作用在人-椅系统上的动压修正系数F的半经验公式。给出选取修正因子ε、f(ε)的方法,仅需4个不同马赫数的阻力系数实验值。原则上,若实验结果精度较高,对阻力系数实验值的选取并无限制。但实验数据精度不高,则上述计算的阻力系数的均方根误差就会大些。此方法不仅适用于计算像人-椅系统这样的大钝体,而且也适用于计算其它大钝体在任意马赫数范围的阻力系数,其均方根误差小于01 05。

关 键 词:弹射座椅  动压  马赫数  风效应  
收稿时间:1993-03-03
修稿时间:1994-01-20

THE CALCULATION PROBLEM OF DYNAMIC PRESSURE ON AIRCREWMAN EJECTION SEAT SYSTEM
Zhang Yunran,Wu Guirong.THE CALCULATION PROBLEM OF DYNAMIC PRESSURE ON AIRCREWMAN EJECTION SEAT SYSTEM[J].Acta Aeronautica et Astronautica Sinica,1995,16(1):70-73.
Authors:Zhang Yunran  Wu Guirong
Institution:Institute of Space Medico-Engineering, Beijing, 100095
Abstract:A new method of calculation that reflects actual situation of the dynamic pressure encountered by seat-man system, particularly at supersonic speeds is presented. Bason on large scale analyses and calculations, a semi-empirical mathematic expression of correction coefficient K of dynamic pressure exerting on seat-man systems is presented and the methods of selecting ε and f (ε) are proposed. For selecting ε and f (ε), only experimental data of drag coefficient at four different Mach numbers are needed. As a principle, the selection of experimental values of drag coefficients is free when the experimental values are of high precision, otherwise its root-mean-square error might be considerable. The present method is not only applicable for the calculation of drag coefficient of large blunt bodies such as seat-man system within arbitrary Mach number range, but also good for other large blunt bodies as well, and its root-mean-square error is less than 0 05. In addition, when the experimental values are expressed as semi-empirical mathematical equation it is convenient for computer programming or simulation under other situations.
Keywords:ejection seats  dynamic pressure  Mach number  wind effects  
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