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“人一舱”热力学数学模型
引用本文:何慧姗,寿荣中,徐小江.“人一舱”热力学数学模型[J].航空学报,1989,10(4):155-163.
作者姓名:何慧姗  寿荣中  徐小江
作者单位:北京航空航天大学 (何慧姗,寿荣中),北京航空航天大学(徐小江)
摘    要: 本文将互相关联的人与座舱环境组成一个大系统,建立了人-舱动态热力学数学模型。模型所用数据系由实验所得,经验公式亦为实验所验证,因而模型具有较高的可靠性。 运用人-舱动态数学模型可以预测飞行员在各种飞行条件下的多种热生理指标,并进而合理确定或检验空调系统的冷却(或加温)能力及各种性能参数。

关 键 词:热生理指标  座舱  热力学  数学模型  
收稿时间:1987-11-30;

DYNAMIC MATHEMATICAL MODEL OF THERMODYNAMICS ON "HUMAN-CABIN
Beijing University of Aeronautics and Astronautics He Huishan,Shou Rongzhong and Xu Xiaojiang.DYNAMIC MATHEMATICAL MODEL OF THERMODYNAMICS ON "HUMAN-CABIN[J].Acta Aeronautica et Astronautica Sinica,1989,10(4):155-163.
Authors:Beijing University of Aeronautics and Astronautics He Huishan  Shou Rongzhong and Xu Xiaojiang
Institution:Beijing University of Aeronautics and Astronautics
Abstract:The dynamic mathematical model of thermodynamics on "human-cabin"has been presented by considering an intergral system of cabin and human.The physiological data used in the model were obtained from tests, and the empirical formulas used in the model were checked with tests.Based on the model, several thermophysiological indexes for the pilot in a cabin can be predicted and the cooling or heating capacity and the other parameters of an air conditioning system can be determined.As an example, the dynamic characteristics of the temperature within the cabin of a fighter in a typical flight profile and the thermophysiological indexes for the pilot set in it were predicted.The finite difference method was applied to computation of the transient temperature within a cabin, and the Roung-Kutta integration scheme was adopted in order to compute thermophysiological indexes of a body tinder varying environmental conditions.The computational results show that the mathematical model presented in this paper is satisfied.
Keywords:human thermophysiological index  cabin  thermodynamics  mathematical model  
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